On the Problem of the Shear Resistance of Wood

Experimental study.
Submitted 1915 | SovietRxiv: ru-191501.07299 | Translated from Russian
Pre-reform orthography. The original is printed in the Russian spelling used before the 1918 reform (ѣ, і, ъ).

Full Text

I. I. Bobarykov.

Professor of the Tomsk Technological Institute of EMPEROR NICHOLAS II.

ON THE QUESTION

OF THE RESISTANCE OF WOOD

TO SHEAR.

Experimental study.

Tomsk.

Siberian Partnership of the Printing Trade, corner of Dvoryanskaya and Yamskoy Lane, own building.

1915.

I. I. Bobarykov.

On the Question of the Resistance of Wood to Shear

Wood is one of the important building materials, and therefore the study of its mechanical properties is of essential importance in construction. Experiments on the resistance of wood to external forces have been carried out since long ago,¹) and at the present time much material can be found for elucidating the question from various sides.

By its nature wood has a very heterogeneous structure, and its resistance to the acting forces depends not only on the kind of deformation, but also on the direction in which it is produced. A whole series of factors sometimes has a very noticeable influence on the numerical values that determine one or another mechanical quality of wood. In addition to the conditions of growth and the time of felling, the position of the specimen being tested in the trunk, the specific gravity, and especially the degree of moisture are of importance.

In accordance with the conditions under which wood is usually subjected to loads in structures, the majority of investigators, in determining the strength of wood, test it in compression, bending, less often in tension and shear, and only in exceptional cases in torsion. It is therefore quite natural that the resistance of wood to compression has been studied best of all for various species, chiefly coniferous ones. It is enough to mention such works as those of Bauschinger,²) Tetmajer,³) Wijkander,⁴) Schwappach,⁵) Jonson,⁶) Janka,⁷) and others.

¹) For example, Chevandier et Wertheim, Sur les propriétés mécaniques du bois, 1846. Barlow, A treatise on the strength of materials, 1867. These works contain some information of a historical character.
²) Untersuchungen über die Elasticität und Festigkeit von Fichten—und Kiefern Bauhölzer, 1883, 1889.
³) Methoden und Resultate der Prüfung der schweiz. Bauhölzer, 1896.
⁴) Untersuchung d. Festigkeits-Eigenschaften schwedischen Holzarten, 1897.
⁵) Untersuchungen über Raumgewicht und Druckfestigkeit d. Holzes wichtiger Waldbäume, 1897.
⁶) Mechanical tests made at Washington University, 1983.
⁷) Untersuchungen über die Elasticität und Festigkeit der österreichischen Bauhölzer, 1900, 1904, 1913.

In structures, wood is very often subjected, in addition to compressive stresses, also to shearing (tangential) stresses; this occurs in bending, in notches, keys, in torsion, in the fastening of disk pins in wooden shafts, etc. The resistance of wood to cutting forces is by no means the same: it is rather considerable if the latter are directed perpendicular to the fibers and, generally speaking, small when the shear is directed parallel to them. This case is of special importance, and therefore most investigators have had it in view in their experiments. Usually, in order to carry out a shear test, a specimen is cut in the form of a prism, which is then subjected to shearing, the plane in which this shearing takes place being directed either radially with respect to the annual rings, or tangentially to them, or obliquely. For example, Tetmayer (see footnote No. 3) used square prisms 4.5–5.5 cm at the base and 10 cm high. The shear planes were directed along 1–1, 2–2, 3–3, 4–4 (Fig. 1); Wijkander took prisms of small height, 20 × 20 cm with a height of 10 cm. Bauschinger (footnote No. 2) divided prisms into four quadrants, from which he obtained eight prisms with triangular and trapezoidal bases (Fig. 2), and the shearing took place along planes I—I and II—II, i.e. in the radial direction. Rudeloff8) cut plates 3 × 4 and 4 × 4 cm, according to Fig. 3; thus the shear planes were either radial or tangential. In Julius’s9) experiments they ran in the tangential direction. A special arrangement occurred in

Fig. 1–3: diagrams of shear specimens and directions.

Fig. 1.  Fig. 2.  Fig. 3.

8) Untersuchungen an Fichtenholz, 1912.
9) The physical characteristics of the hardwoods of Western Australia, 1908.

In Jonson’s experiments (footnote No. 6), shearing here occurred along the planes \(ab\), \(cd\) (Fig. 5). Julius also used the same method, in parallel with Warren’s apparatus. The shearing planes had dimensions of \(1 \times 2\) sq. inches.

Fig. 4.

Fig. 5.

Of the Russian investigations, the most thorough test was carried out by Zhuravsky\(^{10}\); the arrangement of the experiment is shown in Fig. 4.

Either the tenons or the middle part along the planes \(mn\) were subjected to shearing (depending on the dimensions). In the first case \(mn = 8''\), with length \(\delta = 0.2''\), \(b = 0.2''\text{–}0.8''\), width \(a = 0.8''\). In the second arrangement \(mn = 1.5''\text{–}2.6''\), \(a = 0.4\).

In all the experiments indicated, the stress \(k_2\) at failure was determined from the well-known relation:

\[ k_2 = P : F, \]

where \(P\) and \(F\) respectively denote the shearing force and the area of failure. Thus, the law of stress distribution is assumed in advance to be known, namely, a uniform distribution is accepted. This assumption is undoubtedly incorrect, since with the aid of the theory of elasticity it can be shown that the distribution of stresses in shearing follows a more complex law\(^{11}\). The same conclusion as to the impossibility of uniform distributions in shearing must be reached on the basis of logical reasoning. This, among other things, is indicated in the article by V. Mramornov\(^{12}\), who

\(^{10}\) Results of the investigation of the Howe system applied to the bridges of the St. Petersburg–Moscow Railway, 1855.

\(^{11}\) Filon. Philosoph. Transactions of Royl. Society, Series A, V.

\(^{12}\) On stresses in the shearing of wood. 1913. Journal of the Society of Siberian Engineers.

makes an attempt to obtain the desired law and, on the basis of his experiments on shearing, comes to the conclusion that the tangential stresses are distributed according to a hyperbolic law.

Zhuravsky, in the work cited above, says that, according to his observations, the resistance to cutting increases in proportion to the increase of the shearing area only until the length \(mn\) (Fig. 4) becomes equal to 9 times the depth of the notch. With a further increase of this length the resistance does not increase.

In Table I some figures from these experiments are given.

TABLE I.

Length. Depth of notch. Shearing area. Shearing stress. Note.
1.5 in. 0.2 in. 0.12 sq. in. 29.2 lb./sq. in. coarse-grained.
" " " 20.0 " fine-grained.
2.0 " " 0.16 " 25.0 " weak.
" " " 18.1 " strong.
2.6 " " 2.08 " 19.7 " weak.
" " " 13.0 " strong.

Strong coincides with fine-grained. If we take the products of columns 1 and 4, we obtain

\[ \begin{aligned} \text{rows } 1,\,3,\,5\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ 44,\,50 \text{ and } 51.2 \\ \text{” } 2,\,4,\,6\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ .\ 30,\,36.2 \text{ and } 33.8. \end{aligned} \]

Thus, already in Zhuravsky’s experiments one may see indirect confirmation of the non-uniformity of the distribution of stresses.

Of course, the circumstance indicated does not at all devalue the investigations carried out. They give average figures and, in some cases, relations that will hold under any law of stress distribution. For example, in Fig. 6 (see p. 5) a curve is shown depicting the change in the mean temporary resistance to shear of wood with change in the degree of moisture; the diagram is taken from the above-mentioned investigation by Jonson. On the verticals is plotted the degree of moisture in \(\%/\%\), and on the horizontals the stress in pounds per square inch. In general, here the same picture is observed as in compression tests. The resistance increases with ש

with decreasing moisture content; at the same time the influence of the degree of moisture is the more significant, the smaller it is.

Graph showing moisture percentage versus resistance, with plotted points and a curve.

Fig. 6.

In the article “Shearing tests”1 Izod gives figures relating to the resistance of wood to shearing, this being carried out partly in a direction perpendicular to the fibers, simultaneously in two parallel planes, and partly along the fibers. Assuming, as usual, a uniform distribution of stresses, Izod obtained the figures given in Table II, from which we note an enormous difference in the resistance of wood along and across the fibers.

TABLE II.

Wood Weight, cu. ft. Stress, across Stress, along Moisture
Pine 39.5 4872 lb./sq. in. 470 lb./sq. in. 15.7%
Oak 47.7 5292 ” 891 ” 12.6
Spruce 26.5 2668 ” 442 ” 10.6
Yew 45.0 3960 ” 1022 ” 10.0

From the point of view of calculation in structures, knowledge of the average resistance is insufficient, which makes the choice of a factor of safety entirely arbitrary. In the work by V. Mramornov cited above, the author establishes a law of distribution, taking as a basis the assumption that this law does not depend on the length of the sheared portion. In that case, having obtained two points of the required hyperbola, one can find the greatest stress at failure. Without stopping here to consider this method, we deem it necessary to note that in all tests in shearing the phenomenon of bending always occurs, and therefore the results obtained cannot yield absolute figures; the latter must inevitably include an error, which is not so easy to determine.

Shear phenomena are usually studied in torsion, in which it may be assumed with a sufficient degree of accuracy that, in the plane of the cross-section, only shearing stresses develop. According to the law of duality of tangential stresses, the latter must also appear in radial planes. If it is assumed that the law of the straight line according to which the stresses are distributed, reaching a maximum at the periphery, may be admitted also beyond the limits of elastic phenomena, then from torsion tests one can determine the resistance of wood to shear along the fibers; in this case failure will, evidently, occur at the weakest point. Tests on the resistance of wood to torsion have been carried out, but in no considerable number. Thus Bevan, in his article “Experiment of the modulus of torsion”2, gives data for the modulus of elasticity of the second kind \(G\) for several kinds of wood.

TABLE III.

WOOD. Specific weight. Modulus of elasticity. Note.
Acacia 0.795 12850 kg/cm² Not quite dry.
Birch — 7850 Not quite dry.
Chestnut 0.615 10100 Not quite dry.
Scots pine — 6250 Not quite dry.
Larch 0.58 8650 Not quite dry.
English oak — 9100 Not quite dry.
Hamburg oak 0.693 5400 Not quite dry.
American pine — 6720 Not quite dry.
American pine — 6820 Not quite dry.
Poplar 0.333 4330 Not quite dry.
Yew — 7650 Not quite dry.
American yew — 12450 Not quite dry.
Walnut — 9000 Not quite dry.
Pine — 4750 Fresh.

Data on the torsion of wood were obtained by Thurston3. In Table IV are given figures for the temporary resistance to shear for various species.

TABLE IV.

Wood. Stress kg/cm² Note.
White pine . . 107
Yellow “ . 142 sapwood
“ “ . 172 heartwood
Spruce . . . . . 129
Ash . . . . . 184
Red cedar. 137
Oak . . . . . 220
Red wood . 360
Chestnut . . . 142

TABLE V.

Wood. Modulus kg/cm² Stress kg/cm²
Prussian pine . 6893 129.3
“ normal . . 3662 795.0
Oak normal . . 4883 196.0
Elm . . . . 4507 116.0
Beech . . . . . 4507 122.6

One may also point to the article by Bouicseau4, in which are presented the results of torsion tests and the determination both of the modulus of elasticity \(G\) and of the temporary resistance to shear. Table V. The figures presented do not give a sufficiently clear picture of the influence of various factors, such as, for example, the position of the specimen in the tree, the influence of moisture, etc. Therefore there is felt to be a need to set up torsion tests in order to obtain the necessary data on the resistance of wood to shear.

With the intention of proceeding to determine the mechanical properties of construction timber from Tomsk province, chiefly pine and larch, I considered it necessary to include in these tests also the study of resistance to shear. And therefore I decided to set up preliminary torsion tests in order to clarify the circumstances to which attention must be paid. It was proposed to conduct, in parallel, shear tests in order to establish the relation between the stresses in torsion and in shear. Owing to a shortage of material, the task could not be fully carried out.

For carrying out the tests, in the spring of 1912 two trees were acquired at the warehouse of the Administration of State Properties of Tomsk province. According to information received from the Administration, the pines were felled

in the winter of 1911/12 in the Turgai forest along the Chudym River (the right tributary of the Ob River), in the Yuksinskaya allotment; they were delivered on barges in logs 6 arshins long. Each tree yielded two logs. The trees were cut at a height of about one meter above ground level and had a butt diameter of about 12 vershoks, and at the top cut about 9 vershoks. The forest was entirely healthy, with very few knots. In outward appearance the trees differed only somewhat in the average thickness of the annual rings; the tree with the finer layers was 256 years old, the second, with coarser layers, 259 years old. We shall denote them as tree I and tree II.

The cutting for the extraction of specimens was carried out in the same way: the tree was sawn into five boards approximately 60 mm thick; then it was cut perpendicular to the axis into pieces of different heights, 22 pieces in each tree. The numbering of the pieces ran from the top toward the butt. Pieces I, III, VI, IX, XII, XIV, XVII, XX, and XXII, each 426 mm long, served for torsion specimens; pieces V, VIII, XVI, and XIX, each 120 mm long, for compression specimens, and, finally, pieces II, IV, VII, X, XIII, XV, XVIII, and XXI, each 450 mm long, were used for cleavage, bending, etc. From the pieces, by sawing the boards lengthwise, prismatic bars of square cross-section approximately \(60 \times 60\) mm were obtained; moreover, the marking of the pieces for selecting these bars was done with the definite intention of obtaining the greatest possible number of specimens; Fig. 7 gives a diagram of the distribution of specimens in piece III of tree II. The hatched parts were discarded partly as slab pieces, and in the middle of the tree because the principal crack passed there. Specimens 36 and 42 proved, when mounted on the machine, to have small internal cracks, for which reason they were rejected. Thus, only part of the material was necessarily used, though a fairly considerable part; thus, for tree I, of the possible torsion specimens, 18% were unfit, and for tree II—16%.

Fig. 7.

Fig. 7.

The torsion specimens had the form and mean dimensions indicated in Drawing 8. The tests were carried out on an Amsler machine, which was checked before and after the investigation. The mean diameter of the specimens

Drawing 8.

was equal to \(d = 50\) mm. On the cylindrical part of the bar, two marks were made at a distance \(l = 150\) mm from one another; mirrors were fastened at these sections, by means of which the elastic angles \(\alpha\) of twist were read, and with change of the twisting moment by 2 kg·m. From these data the value of \(G\) was determined from the formula

\[ G = \frac{32}{\pi}\frac{Ml}{\alpha d^4}. \]

Strict proportionality between stress and deformation was not observed in all bars, as may be seen, for example, from Drawing 9, which shows diagrams obtained for specimens Nos. 43, 119, 142, 169, and 189 of wood No. I (Table A). Whereas for specimen No. 119 this relation is represented, although with very large radii of curvature. As an example we give two records.

Specimen Load Difference of scale readings
Wood I. 2.1 kg·m 1.33 cm/m
Section III. 4.2 1.30
Specimen No. 27. 6.0 1.30
8.0 1.30
10.0 1.30
12.0 1.60
23.0 failure
Wood I. 2.0 kg·m 1.20 cm/m
Section III. 4.0 1.20
Specimen No. 35. 6.0 1.23
8.0 1.25
10.0 1.26
12.0 1.45
20.5 failure

Owing to the circumstance indicated, it must be acknowledged that the modulus of elasticity \(G\) varies, decreasing with the load; but since this decrease is insignificant, it is possible to compute \(G\) as an average quantity; the stresses were computed by the formula

\[ k=\frac{16M}{\pi d^{3}}. \]

The elastic limit was not determined; assuming that it lies not far from the proportional limit, the stresses \(k_1\) corresponding to this latter limit were computed. It is self-evident that the value of these figures is approximate, on the basis of what has been said above.

The quantities \(k_1\) and \(k_2\)—the stress at failure—are placed in Tables A and B (see the appendix).

After failure, which was determined by the drop of the load on the machine and the appearance of a longitudinal crack, a cylinder was immediately cut from the middle of the specimen, with a diameter corresponding to the diameter of the specimen and with a height of about 30 mm (on the average). This cylinder was weighed and then subjected to drying at a temperature of about \(98^\circ\) C.\(^{17}\) In this way the degree of moisture \(\varphi\) at the moment of carrying out the experiment was found. In addition, knowing the weight of the dried cylinder, the specific gravity of the specimen was determined. The volume was obtained by direct measurement; this method was preferred to the method of immersion in liquid, because the former is simpler; the degree of error in both methods is approximately the same. The average thickness of the annual rings was obtained by dividing the diameter of the cylinder by the number of rings counted in the given cylinder.

In Tables A and B all these data are presented.

As we see, the moisture content of the wood (regarding the specimens dried in the oven as absolutely dry) varies within the limits of \(6\)—\(13.5\%\); the humidity in the laboratory room varied, depending on the state of ventilation, from 40 to 50% on the average.

With such a comparatively small water content, it may be assumed that the specific gravity varies proportionally to the change in moisture. Let the specific gravity be denoted by \(\Delta\); then we shall have

\[ \frac{\Delta-\Delta_o}{\varphi-\varphi_o}=Const.=A, \]

where \(\Delta_o\) and \(\varphi_o\) refer to absolutely dry wood, but \(\varphi_o=0\). As is seen from column 6 of Tables A and B, the indicated ratio varies very little.

\(^{17}\) In a cabinet with double walls, between which distilled water boiled.

Below are given the mean values for all sections of the trees tested:

Section Tree I Tree II
1 0.251 0.248
3 0.246 0.254
6 0.245 0.256
9 0.256 0.249
12 0.236 0.261
14 0.234 0.265
17 0.234 0.254
20 0.266 0.260
22 0.240 0.260
Average 0.245 0.257

On the basis of (4) we may write

\[ \Delta = A \varphi + \Delta_o \]

\[ \Delta_1 = A \varphi_1 + \Delta_o \]

or

\[ \Delta_1 = \Delta - A(\varphi - \varphi_1) \]

Let, for example,

\[ \varphi_1 = 10\%, \]

then

\[ \Delta_1 = \Delta A(\varphi - 10) \]

For tree II, \(A = 0.257\); in such a case we obtain

\[ \Delta_{10} = \Delta + 2.57(1 - .01\varphi). \tag{19} \]

Thus we have the possibility of referring the data obtained to a moisture content of \(10\%\) and then comparing them with one another. Let us see what the error will be if the numerical values of the specific gravity are left without reduction. For tree II we have

\[ \varphi_{max.} = 12.7\% \;(\text{No. }70), \quad \varphi_{min.} = 6.8\% \;(\text{No. }125), \quad \Delta_{min.} = 36.3 \]

and according to (6) we have

\[ \Delta'_{10} = 36.3 + 2.57(1 - 0.1 \cdot 12.7) = 35.6 \]

\[ \Delta''_{10} = 36.3 + 2.57(1 - 0.1 \cdot 6.8) = 37.2 \]

and

\[ \frac{\Delta''_{10} - \Delta'_{10}}{\Delta}\,100 = 4.2\%. \]

Consequently, the greatest deviation does not exceed \(4.2\%\), but since such a simultaneous coincidence of unfavorable circumstances does not

observed, the actual error due to neglecting the influence of moisture will not exceed 2%. Therefore no reduction of the specific gravity to any definite degree of moisture was made.

It may be supposed that a change in moisture within the comparatively small limits of 6–7% should not be strongly reflected in the magnitude of the temporary resistance. Turning to the diagram indicating the dependence between \(k_2\) and \(\varphi\) according to Jonson’у (Fig. 6), we note that the temporary resistance falls sharply with increasing moisture, and this is especially noticeable at small values of \(\varphi\). A similar phenomenon was also observed by Janka in the curves he constructed for the case of compression. In order to form an idea of the actual influence of a change in \(\varphi\) under torsion, I made special observations. Namely, from logs 4, 15, and 21—wood I—and 7, 11, and 18—wood II—small beams were selected. From each small beam two specimens for torsion were prepared in the form indicated in Fig. 8, but of considerably shorter length. This was done with the aim of having paired specimens, situated as close as possible to one another along the length and, consequently, possessing approximately the same specific gravity and moisture.

After fabrication, one small beam was set in the machine, while the other was at the same time placed in a drying cabinet to determine the degree of moisture. After drying was completed, the second small beam, which had been kept in a desiccator, was subjected to torsion. In this way, for each small beam from the log, two figures were obtained—the temporary resistance at a certain degree of moisture and in an absolutely dry state. The results of these tests are collected in Tables \(C\) and \(D\), corresponding to woods I and II. Looking through the figures found, we note, first, that the resistance of wood to shear by no means always decreases with increasing moisture; for the case under consideration the opposite relation may occur. The greater part of the specimens showed a lower stress in shear in the completely dry state6. Secondly, the fluctuations in the change of the magnitude, together with drying, are rather considerable and do not reveal any definite law of the phenomenon. The result obtained is, to a certain extent, in contradiction with the accepted views on the influence of moisture. Of course, I cannot draw an exact conclusion on the basis of the available material, but I believe that there is no reason to consider impossible a decrease in resistance at very small degrees of moisture; it is necessary

one must keep in mind that under these conditions the wood becomes little elastic and, to a considerable degree, brittle. The curves shown in drawing 9 were obtained precisely in the last experiments and give diagrams for wet (a) and dry (b) specimens from wood I. Returning to Tables C and D, let us determine the mean values of the ratio

\[ m=\frac{k_2-k'_2}{\varphi}, \]

where \(k_2\) and \(k'_2\) are the temporary resistance for wet and dry specimens. We shall have

Wood I.

Cut 4—\(m=0.31\) kg/cm.\(^2\)

” 15—\(m=0.70\) ”

” 21—\(m=0.93\) ”

Wood II.

Cut 7—\(m=0.94\) kg/cm.\(^2\)

” 11—\(m=1.03\) ”

” 18—\(m=1.40\) ”

It is easy to see that the decrease in resistance per 1% of moisture increases, approximately, from the top toward the butt. Plotting, on a chosen scale, distances along the axis of abscissas, and the values of \(m\) vertically, we obtain two straight lines I and II, i.e. it may be assumed that \(m\) varies inversely proportionally to the distance from the soil level.

In such a case the greatest decrease per 1% of moisture will be 1.6 kg/cm. for cut 22 of wood II.

If we take as the normal moisture content \(\varphi = 10\%\), then specimen No. 252 will have the greatest deviation from this mean value,

Figure 10.

Fig. 10.

whose moisture content was \(\varphi = 7\%\). The stress, reduced to the normal moisture content for this specimen, would be

\[ k_{10} = k - m(10 - \varphi) = 87.5 - 3 \cdot 1.6 = 82.7 \ \text{kg}/\text{cm}^2, \]

which corresponds to a deviation of \(5.5\%\).

Not having in view, in the present work, the obtaining of exact dependences, I did not reduce the obtained stresses to a single moisture content of \(10\%\). But it is self-evident that, in a further investigation of the phenomenon of shearing of wood, it will be necessary to keep the indicated circumstance in mind.

As for clarifying the question of the influence of the degree of moisture content on the modulus of elasticity, special experiments in this direction were not carried out, because it was difficult to dry long specimens; moreover, over the length of one meter one cannot speak of constant moisture content and specific gravity. To determine the change in the magnitude \(G\) together with \(\varphi\), it is necessary to arrange the experiments in a somewhat modified form.

If, using the data of Tables A and B, one compiles the mean values for each section, then Tables VI (wood I) and VII (wood II) are obtained.

TABLE VI.

Section Specific weight Thickness of annual layer, mm Modulus of elasticity, kg/cm² Stress \(k_1\), kg/cm² Stress \(k_2\), kg/cm²
1 0.384 0.72 6160 43.3 74.2
3 0.394 0.71 6130 47.2 78.0
6 0.420 0.73 6420 46.7 77.5
9 0.417 0.75 6580 46.5 80.5
12 0.460 0.75 6900 49.3 75.2
14 0.455 0.75 7620 51.6 82.4
17 0.478 0.77 7550 52.3 89.1
20 0.506 0.79 7590 51.1 90.7
22 0.523 0.83 8400 61.3 102.5

TABLE VII.

Section Specific weight Thickness of annual layer, mm Modulus of elasticity, kg/cm² Stress \(k_1\), kg/cm² Stress \(k_2\), kg/cm²
1 0.396 0.88 6940 43.6 76.0
3 0.408 0.88 7220 42.9 78.6
6 0.410 0.89 6940 41.5 74.9
9 0.416 0.89 7180 45.3 81.0
12 0.426 0.87 7880 49.8 84.0
14 0.443 0.90 8050 50.0 85.0
17 0.458 0.96 7540 50.5 82.0
20 0.474 0.98 7690 52.0 82.3
22 0.500 1.00 8830 55.7 98.0

For clarity, the changes in these quantities together with the change in the distance of the section from the butt are presented in the form of curves in Fig. 11 (tree I) and Fig. 12 (tree II). Here the general law is confirmed that the specific weight of the tree increases as one approaches the butt, with the increase being greatest in the last section. Here, incidentally, the greatest resin content also appears. Approximately parallel to the curve of specific weight run the curves of temporary resistance and of the modulus of elasticity. This circumstance suggests that between the quantities \(G\), \(k\), and \(\Delta\) there exists a certain constant relation. Indeed, from Tables VI and VII we find.

TABLE No. VIII.

Segment Tree I: \(g : k_2\) Tree I: \(k_2 : 100\Delta\) Tree I: \(k_2 : k_1\) Tree II: \(g : k_2\) Tree II: \(k_2 : 100\Delta\) Tree II: \(k_2 : k_1\)
1 8.27 1.93 1.77 9.13 1.92 1.74
3 7.80 1.98 1.65 9.19 1.92 1.83
6 8.29 1.85 1.67 9.27 1.83 1.80
9 8.31 1.90 1.70 8.87 1.95 1.78
12 9.18 1.64 1.52 9.33 1.96 1.69
14 9.29 1.80 1.61 9.46 1.92 1.70
17 8.47 1.86 1.70 9.20 1.84 1.63
20 8.36 1.80 1.78 9.33 1.74 1.58
22 8.19 1.96 1.67 9.04 1.95 1.75
Average 8.47 1.86 1.68 9.20 1.89 1.72

Thus, one may take approximately, for both trees,

\[ k_2 \approx 1.7\,k_1 \quad \text{and} \quad k_2 \approx 190\,\Delta. \]

As was indicated above, the resistance of wood to compression has been studied sufficiently well for many of its varieties. It is therefore of undoubted interest to determine what relation exists between the resistance of pine to shear and to crushing. When cutting up the trees, these tests were provided for, and for them four sections were set aside. From these, bars 12 cm long were sawn out, with a square base \(6 \times 6\ \mathrm{cm}^2\), i.e. the ratio of height to the side of the base was taken equal to 2. This height was chosen deliberately, so as to make it possible to set up a delicate apparatus for finding the modulus of elasticity \(E\) of the first kind. Crushing was carried out in Amsler’s press, of 60-ton capacity. The deformations were read by means of Bach’s sector instrument. The results obtained are collected in Tables E and F, respectively for Trees I and II. The stresses, as well as the modulus of elasticity, increase with approach to the butt.

If the mean data by sections are calculated, Table IX is obtained.

Fig. 11.

Visible graph labels: \(G\), \(K_2\), \(K_1\), \(\Delta\); ordinate markings include \(8000\), \(7000\), \(6000\) with units \(k/c^2\), and \(100\), \(80\), \(60\), \(40\), \(20\) with units \(k/c^2\); additional markings \(0.5\), \(0.4\); abscissa markings \(0, 1, 2, 3, 4, 5, 6, 7\), \(m\).

Fig. 12.

(Graph with curves labeled \(\xi\), \(K_2\), \(\Delta\), and \(\delta\); horizontal axis \(m\). Visible scale labels include \(9000\ \mathrm{K}/\mathrm{c}^2\), \(6000\), \(100\ \mathrm{K}/\mathrm{c}^2\), \(80\), \(60\), \(40\), \(20\), \(0\), as well as \(0.4\), \(0.3\), \(1^\circ\), and \(0^\circ 9\).)

Graph with plotted curves labeled \(E\), \(K_2\), \(g\), \(K_s\), and \(\delta\).

Fig. 13.

TABLE IX.

Log section Wood I: stress \(k_1\), kg/cm² Wood I: stress \(k_2\), kg/cm² Wood I: modulus, kg/cm² Wood II: stress \(k_1\), kg/cm² Wood II: stress \(k_2\), kg/cm² Wood II: modulus, kg/cm²
5 350 486 72000 360 505 70070
8 340 492 74000 358 531 76000
16 423 639 88600 345 566 87100
19 374 664 95600 365 636 101100

As was to be expected, the resistance of the wood increases from the top log section toward the butt. The same is also observed with the modulus of elasticity. In drawing 13 the changes in the quantities \(E\) and \(k_2\) are shown with the change in position relative to the butt. The dotted lines refer to wood I, the solid lines to wood II. For clarity, on the same drawing are plotted lines representing the changes in the modulus of elasticity of the second kind \(G\), the temporary resistance to shear \(k_s\), and the thickness \(\delta\) of the end rings. These quantities were taken for the log sections 6, 9, 17, and 20, nearest to 5, 8, 16, and 19. The direction of the lines indicates the relation among the quantities represented. The stress \(k_1\), corresponding to the limit of proportionality, is calculated approximately, in view of the circumstances that were mentioned in connection with the torsion tests. It is not without interest to note that the ratio between the temporary resistance in compression and in torsion is approximately constant and is equal to the ratio between the stresses at the limit of proportionality. This can be seen from the following Table X, which gives a comparison of the indicated ratios. To make comparison possible, the mean data have been taken for specimens coinciding in direction in two neighboring log sections, in compression and torsion.

TABLE X.

Log section: compression Log section: torsion Wood I: limit of proportionality Wood I: failure Wood II: limit of proportionality Wood II: failure
5 6 7,5 6,3 8,0 7,3
8 9 7,3 6,2 7,9 6,4
16 17 7,4 7,2 6,8 6,9
19 20 7,4 7,4 7,0 7,7
Mean 7,4 6,8 7,3 7,1

i.e., on average it comes out to about seven.

Finally, comparing in the same way the moduli of the first and second kind with one another, we observe that the ratio between \(E\) and \(G\) fluctuates comparatively little, increasing from the cut end toward the butt.

Drawing 14.

TABLE XI.

Cut. Compression Cut. Torsion Wood II. \(E:G\) Wood I. \(E:G\)
5 6 10.8 10.2
8 9 11.8 10.6
16 17 11.2 11.5
19 20 12.3 13.2

and on average it may be taken as about 11.

Wishing to make use of the results of the torsion tests in phenomena of shear, it is necessary, for comparison, to have figures for resistance to shear obtained from a direct test upon it. It was indicated above that it is impossible to put such observations in pure form, since shear is inevitably accompanied by bending. Moreover, owing to the uncertainty of the law of distribution of stresses, one can obtain only a mean value for the quantity \(k_2\). It was therefore decided nevertheless to make several tests in order to obtain such figures. First the specimen was given the form shown in Drawing 14. A bar of square section (approximately \(6 \times 6\)) had thinner parts \(A\) and \(B\), which served for gripping in the machine. Perpendicular to the fibers, on opposite sides, saw-cuts \(aa\) were made, with the calculation that, under the action of the forces \(P, P\), sliding would occur along the plane \(AB\). The length of splitting was 100 m/m. At the points \(c, c, c, c\), at a distance of 2 cm from one another, mirrors were installed. The latter were fastened in a support having the form indicat-

to that in Fig. 15, and, in order to reduce its weight, made of aluminum; the collar \(b\) could rotate on a pin forming one whole with the base \(a\); into the latter were set needles \(d, d\), representing feet; by sticking the latter into the wood, they fixed the position of the mirror. The distance between the feet was 3 mm. The mirrors were set so that the shearing line passed between the needles. By means of tubes with scales, placed at a distance of 2 meters from the mirrors, readings were observed which were the result of the combined action of shear and skewing (the work was carried out on a 2-ton Amsler machine). The loading began at 50 kg and, increasing at each observation by 100 kg, after the reading was reduced to 50 kg. The greatest load was \(P = 550\) kg. From the results obtained, the arithmetic means were taken, i.e., the readings at 100 kg. In order to eliminate the influence of skewing, after the end of the test in the form described, at a load of 50 kg, the mirrors were removed and again set at the same points \(c\text{—}c\), but with the base turned through \(90^\circ\), i.e., in the new position the needles were arranged along the line \(AB\) between the saw cuts (Fig. 14). Then loading and unloading proceeded in the same way as before; average figures were computed, which were, of course, smaller than the first ones. The differences obtained by subtracting the corresponding figures of the second series from the figures of the first were accepted as quantities proportional to the shear deformations, since the phenomenon took place within the limits of elasticity. In order to be certain that an analogous phenomenon took place on the other side of the bar, a mirror was set at point e-5, corresponding to c-1. The conduct of the tests required great effort because of the painstaking and difficult installation of four mirrors and tubes in such a small space; all observations were repeated. The results of tests on 6 specimens showed that the largest readings are given by the end mirrors, as is seen from the following Table XII.

Fig. 15.

TABLE XII.

No. Difference of mirror readings Difference of mirror readings Difference of mirror readings Difference of mirror readings Difference of mirror readings
1 2 3 4 5
1 0.3 0.2 0.3 0.7 0.7
3 0.8 0.1 0.3 0.8 1.0
19 0.4 0.1 0.0 0.3 0.4
30 1.1 0.2 0.2 0.6 0.6
47 1.2 0.4 0.7 1.0 0.9
70 1.3 0.5 0.3 0.8 0.7

If these quantities are laid off, on the chosen scale, assigning them to points 1–9, we obtain the curves shown in Fig. 16. Since these curves do not make it possible to derive a definite law of stress distribution, further experiments in this direction were discontinued, in order to single them out as an independent problem. It is thought, nevertheless, that the result obtained may be regarded as sufficient to establish the presence of a maximum of stresses at \(a\) and \(b\) and a minimum in the middle.

Fig. 16.

The experiments just described confirmed the presence of skewing of the beams, and to a fairly considerable degree.

Wishing to weaken the influence of this circumstance on the resistance in shear, the following observations were made on beams of a somewhat different shape—namely, prepared according to the type shown in Fig. 17. Here splitting must occur simultaneously along the planes \(bc\)—\(bc\), over a length likewise of 100 mm. Comparing the forms of Figs. 14 and 17 with one another, it is easy to see that, all other conditions being equal, the bending moment in the latter case will be approximately 60% smaller and, of course, cannot be eliminated altogether. The number of specimens for splitting could not be made large, since here it was necessary to locate the plane of splitting in a perfectly definite manner, so as to guarantee the phenomenon in a more or less proper form.

Fig. 17.

A whole series of beams had to be rejected, because during failure extraneous phenomena appeared, such as, for example, the tearing of some—

rupture of fibers, shear in an oblique direction, waviness of fibers, etc. All these circumstances artificially increased the resistance of the wood.

TABLE XIII.

Specimen, shearing Specimen, torsion Stress, shearing Stress, torsion Ratio Specimen, shearing Specimen, torsion Stress, shearing Stress, torsion Ratio
No. 2 No. 2 17.1 78.1 4.56 88 86 18.2 94.5 5.19
5 4 15.0 65.5 4.36 89 89 20.2 91.9 4.54
7 6 17.9 81.1 4.53 90 88 19.5 91.9 4.72
9 7 15.3 75.5 4.93 92 90 16.2 79.8 4.92
10 8 14.8 61.7 4.16 96 94 20.0 77.7 3.89
11 9 17.8 84.0 4.72 97 95 14.0 70.3 5.02
14 11 15.9 68.7 4.33 101 98 18.8 87.2 4.63
15 12 17.4 62.7 3.60 102 99 16.7 65.7 3.93
18 16 20.0 71.2 3.56 104 100 17.0 65.2 3.83
26 25 17.3 67.4 4.02 105 101 19.7 69.5 3.54
28 27 19.3 87.0 4.50 114 110 18.3 89.2 4.86
37 38 18.0 89.3 4.96 116 112 13.2 67.9 5.14
44 42 16.3 57.0 3.50 117 111 19.0 87.4 4.60
45 43 18.0 74.4 4.13 123 118 18.1 88.0 4.86
48 46 13.5 63.3 4.68 125 121 25.2 106.8 4.24
55 53 17.3 88.1 5.09 128 125 16.3 72.0 4.41
62 60 18.0 74.5 4.14 133 128 15.0 62.0 4.13
69 67 20.0 90.7 4.53 135 130 18.6 97.5 5.24
70 68 19.4 77.2 3.98 137 132 18.5 93.5 5.05
71 69 20.5 90.1 4.45 139 137 23.7 91.0 3.84
72 70 20.4 79.7 3.90 145 141 18.4 82.0 4.45
73 71 16.9 80.7 4.66 150 146 20.3 76.2 3.75
78 76 17.7 91.5 5.17 153 149 16.6 76.0 4.58
79 77 21.3 61.3 3.63 156 154 15.3 73.3 4.78
80 78 19.7 83.6 4.25 161 158 22.4 80.0 3.57
81 79 14.3 55.7 3.89 167 165 22.5 88.6 3.94
83 81 18.4 82.0 4.25 166 164 22.0 95.7 4.34
86 84 16.9 71.2 4.71 172 169 17.5 61.0 3.40
87 85 15.0 62.9 4.20 178 175 21.5 91.8 4.26
Average 4.36

Table XIII gives the results obtained for 58 specimens of wood I, taken, as is seen, from different cuts, i.e. at different heights. For each specimen in tension (cleavage) a specimen from an adjacent cut for torsion, lying in the same direction, was selected. It may be observed that the ratio $\gamma$ between the temporary resistances for torsion and for tearing out (the mean value), although not constant, fluctuates only slightly. This circumstance confirms the correctness of the assumption that the strength of wood with respect to shearing can be determined from torsion tests. Unfortunately, the figure for the mean temporary resistance obtained from cleavage tests cannot characterize the magnitude of the resistance, since it depends on the length of the cleaved portion (up to a known limit). Therefore the ratio found in Table XIII is also correct for a cleavage length of 100 m/m, but

taking into account that for each tree one can find that limiting length of shearing beyond which the magnitude of the mean resistance already remains unchanged, it is evidently possible to obtain such a value of \(\eta\) as will characterize the given kind of timber.

The theory of plane bending indicates that, under this kind of deformation, tangential stresses develop in the material of the bar. If one selects a form of cross-section such that failure occurs as a result of the development of large shearing forces, then it would be possible to calculate the magnitude of the temporary resistance by yet another method. Wishing to make use of this circumstance, it was decided to prepare specimens for bending tests from bars 2 and 21 of tree II. For this purpose three specimens were cut from each bar; the cross-section had the form of an I-beam (Fig. 18), with a small web height and with thickened flanges; the dimensions \(a = 14—15\) mm, \(h = 25\) mm, \(b \approx 5\) mm, \(c = 6—7\) mm were chosen so that failure would occur as a result of shearing along the neutral layer.

Fig. 18.

The bending of the specimen was carried out in such a way that it was placed on two supports with a span of 140 mm. The force \(P\) was applied at the middle of the bar; the load was gradually increased until failure. The stresses were calculated according to the known relation

\[ k = \frac{3P\left(ah^2 - b^2(a-c)\right)} {4\left(ah^3 - (a-c)b^3\right)c}. \]

The results of these determinations are given in Table \(G\). Each stress figure is the mean of three parallel tests on material from one and the same bar. Sections 2 and 21 are situated between sections 1 and 3, and 20 and 22, the bars from which served as material for the torsion tests. If one takes the mean values of the stresses in the specimens of sections 1, 3, 20, and 22 corresponding to the specimens of Table \(G\), and compares them with the mean values of the latter, the following table is obtained.

TABLE XIV.

Section Specific gravity Stress \(k_s\) Ratio
II 0.396 91.5 kg/cm\(^2\)
I—III 0.403 77.0 ” 1.19
XXI 0.482 108.2 ”
XX—XXII 0.487 90.1 ” 1.20

For cuts located at opposite ends of the tree, we obtain one and the same ratio between the stresses found from bending tests and from torsion tests. The former turns out to be 20% higher than the latter stress. A difference of this kind is very simply explained by the presence of friction, which must be overcome in order to destroy the beam by bending. For compression we do not know the coefficient of friction and cannot introduce the corresponding correction. An approximate consideration permits us to think that the friction force will be approximately about 20% of the magnitude \(k\).

If the law of stress distribution is taken to be a hyperbola, then from the shearing experiment one can derive the value of the greatest temporary resistance. At my request V. Mramornov carried out several experiments on small boards taken from different places in tree II. The shearing surface was marked out as in the beam shown in Fig. 14, but of small thickness. The line \(AB\) had to run along one and the same layer.

Each figure is the average of 2–3 observations. The number of experiments is not large, since there was no longer enough material, and chiefly because it is very difficult to select strictly straight-grained beams, as a result of which many of them were rejected. In order that the figures obtained in this way could be compared with the data found from torsion tests, corresponding pieces for torsion were sought for each beam; at the same time the condition was imposed that, as far as possible, the beams being compared should lie in one direction along the length of the tree. Table XV gives the results of the indicated experiments.

TABLE XV.

Shearing: cut Shearing: specimen Shearing: stress, kg/cm² Torsion: cut Torsion: specimen Torsion: stress, kg/cm²
IV 25 81 VI 53 80.0
IV 26 78.0 VI 54 83.4
IV 28 77.0 VI 56 69.9
IV 32 69.6 VI 60 72.0
IV 33 81.5 VI 64 85.0
IV 37 77.0 VI 68 82.5
IV 38 86.0 VI 44 87.0
IV 43 86.0 VI 49 75.0
IV 45 84.8 VI 51 84.0
X 76 83.6 IX 85 87.5
X 77 81.0 IX 81 79.6
X 90 88.4 IX 106 98.0
X 91 76.3 IX 107 71.6
XIII 129 82.8 XIV 153 89.4
XVIII 189 98.0 XVII 194 93.8
XXII 231 105.0 XXII 232 97.2
XXII 254 108.0 XXII 263 109.5
XXII 260 107.0 XXII 259 116.5

It is self-evident that one can no longer expect complete agreement, because wood is far too inhomogeneous a material. But the difference established from Table XV is not great, and in any case gives grounds to suppose that experiments in this direction are desirable.^21)

There may also arise the question of the change in the magnitude of this temporary resistance in the cross section with change in distance from the center. In this respect it should be noted that it is impossible to establish an entirely exact regularity. In Fig. 19 diagrams are given showing the course of the values \(k_2\) (solid lines), specific gravity \(\Delta\) (small dash), and \(G\) (large dash) for sections 1, 3, 6, 9, 12, 14, and 17 of tree I, and 1, 3, 6, 12, and 17 of tree II. The direction is taken from the center of the section toward the south. In Fig. 20 analogous diagrams are given for sections 1, 12, and 22 of tree I, and 3, 12, and 17 of tree II; the direction is from the center toward the east.

In general the following peculiarity is observed: the temporary resistance does not follow the change in specific gravity, but rather the reverse; meanwhile, when examining the changes along the length of the trunk, we noted the circumstance that the temporary resistance increases together with the increase in specific gravity (Fig. 11). Further, the smallest value of the temporary resistance along the radius is obtained between the heartwood and the sapwood. Approximately the same is observed also in the diagrams of Fig. 20.

What has been set forth above may lead to conclusions of the following kind. The torsion test gives the magnitude of the least resistance to shear; the temporary resistance \(k_2\) changes with position in the trunk; between the temporary resistance to torsion and to compression there may exist a simple dependence, just as between the moduli \(E\) and \(G\) for one and the same tree. In experiments for determining the mechanical properties of wood it is desirable to conduct parallel torsion experiments, and in this connection it is necessary to clarify the influence of the degree of moisture on the various factors that determine these mechanical properties.

I consider it my duty to express my gratitude to my assistant in the mechanical laboratory of the Tomsk Technological Institute, mechanical engineer A. P. Malyshev, who gave me great assistance in carrying out the experiments.

I. Bobarykov.

April 1914
Tomsk.

^21) Such a study is also being planned in the Mechanical Laboratory of the Tomsk Technological Institute in the near future for oak, larch, and birch.

Wood I

  • Experiment No. 1
  • Experiment No. 5
  • Experiment No. 6
  • Experiment No. 9

  • Experiment No. 8

  • Experiment No. 14
  • Experiment No. 7
  • Experiment No. 1

  • Experiment No. 3

  • Experiment No. 9
  • Experiment No. 12
  • Experiment No. 17

Axis markings visible on the diagrams include: \(0.2,\ 0.4,\ 0.6\); \(20,\ 40,\ 100,\ 160\); \(5000,\ 6000,\ 7000,\ 8000,\ 9000\); and \(kg/cm^2\).

Wood II.

Fig. 11.

Chart 20. Legend: dashed line — Э; dotted line — Δ; solid line — K. Wood I and Wood II; ordinate labels “shear” (kg/cm²) and “shear” (kg/cm²); abscissa in m/m.

Table A.

Sample Specimen Specific gravity, wet Specific gravity, dry Humidity, % Ratio \(100(\Delta_1-\Delta)/\varphi\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Thickness of annual layer, mm Note
I 2 0,418 0,390 11,2 0,270 35,3 78,1 8240 0,42
I 3 0,408 0,380 11,3 0,245 43,2 74,4 5295 0,44
I 4 0,412 0,382 12,7 0,236 — 65,5 — 0,81 Knot.
I [[unclear]] 0,403 0,383 11,0 0,210 43,9 63,0 6745 0,52
I 6 0,407 0,378 11,1 0,261 42,7 81,1 5590 0,44
I 7 0,409 0,380 10,6 0,273 34,0 75,5 5075 1,08 Knot.
I 8 0,419 0,391 10,4 0,269 40,5 61,7 ? 1,35
I 9 0,415 0,391 10,9 0,220 38,8 84,4 5430 0,41
I 10 0,413 [[unclear]] 7,8 0,256 45,8 85,5 5945 0,54
I 11 0,413 0,382 10,8 0,287 34,4 68,7 8120 1,51
I 12 0,424 0,400 10,1 0,238 41,5 62,5 7690 0,72
I 13 0,373 0,349 9,3 0,258 35,3 74,3 5285 0,57
I 14 0,427 0,401 10,2 0,234 34,0 62,3 6100 0,70 Small crack.
I 16 0,407 0,377 10,4 0,238 40,5 71,2 5370 1,11
I 17 0,441 0,420 11,1 0,217 48,3 83,3 6505 0,73
I 18 0,389 0,367 9,4 0,234 51,6 81,3 5550 0,55
I 19 0,419 0,397 9,3 0,258 33,7 67,5 5415 0,5?
I 20 0,404 0,378 8,9 0,292 50,6 84,4 6325 0,52
III 21 0,461 0,440 7,2 0,293 36,0 70,0 5910 0,70
III 22 0,429 0,410 7,6 0,230 49,0 74,0 7550 0,40
III 24 0,393 0,374 8,0 0,238 45,3 80,4 6627 0,44
III 25 0,416 0,394 9,0 0,244 57,4 75,8 4160 0,82
III 26 0,395 0,375 9,0 0,222 42,6 69,5 6130 1,10
III 27 0,425 0,406 8,4 0,226 56,0 87,10 5963 0,50
III 31 0,420 0,400 8,7 0,230 43,0 75,5 6163 0,88
III 32 0,380 0,360 8,1 0,247 48,0 92,0 6027 0,55
III 33 0,387 0,367 7,7 0,260 56,3 72,3 6070 0,44
III 34 0,395 0,377 8,4 0,227 37,4 82,0 5860 1,73
III 35 0,465 0,444 7,1 0,295 49,5 74,0 6305 0,86
III 36 0,392 0,378 6,5 0,216 47,7 81,4 5290 0,53
III 38 0,433 0,419 6,5 0,216 56,0 89,3 6310 0,75
III 39 0,452 0,435 7,1 0,230 53,3 85,0 5780 0,81
III 40 0,385 0,368 6,8 0,250 44,1 82,0 6310 0,50
III 42 0,381 0,364 6,5 0,262 35,0 57,0 6000 0,50
VI 43 0,457 0,437 10,6 0,283 43,7 74,4 6060 0,42
VI 44 0,475 0,458 8,8 0,250 63,5 90,0 6415 0,44
VI 45 0,448 0,427 10,0 0,210 43,5 80,0 6100 0,44
VI 48 0,477 0,450 9,4 0,286 46,5 63,3 5175 1,16
VI 51 0,420 0,400 8,0 0,250 45,5 92,7 6250 0,44 Resin pocket.
VI 52 0,426 0,405 8,6 0,244 53,5 70,0 5370 1,19
VI 53 0,450 0,428 9,1 0,242 37,8 88,1 6200 0,88
VI 54 0,402 0,377 9,9 0,253 43,0 75,3 6820 0,60
VI 55 0,438 0,415 10,9 0,211 56,4 82,1 6020 0,45
VI 56 0,437 0,417 8,2 0,244 36,0 76,0 5490 1,72
VI 57 0,478 0,458 9,4 0,213 32,3 70,6 5450 1,04
VI 58 0,414 0,392 9,6 0,229 43,5 85,0 6125 0,51
VI 60 0,460 0,439 9,5 0,221 28,6 52,4 5645 0,72
VI 61 0,440 0,410 10,6 0,283 48,0 63,0 7445 1,06 Knot in the head.
VI 62 0,470 0,436 10,6 0,323 44,3 74,5 8070 0,82
VI 63 0,425 0,399 10,5 0,247 58,6 77,2 5930 0,50
VI 64 0,470 0,439 10,6 0,292 45,9 75,3 8430 0,69
VI 65 0,461 0,434 11,0 0,245 58,6 86,3 8020 0,57
VI 66 0,421 0,398 10,3 0,223 48,0 80,0 6360 0,55
VI 67 0,432 0,405 10,8 0,250 57,9 90,8 7130 0,47
VI 68 0,457 0,434 11,0 0,209 46,9 72,2 6200 0,60
Cut Specimen Specific gravity, wet Specific gravity, dry Moisture, % Ratio \(100(\Delta_1-\Delta)/\varepsilon\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Thickness of annual rings, mm Note
IX 69 0,436 0,407 10,8 0,268 46,9 90,1 6200 0,52
IX 70 0,443 0,416 10,5 0,267 58,3 79,7 5560 0,54
IX 71 0,472 0,438 11,7 0,290 44,0 80,7 7370 1,07
IX 72 0,432 0,417 7,1 0,212 53,8 65,1 5820 1,35
IX 74 0,426 0,399 10,8 0,250 58,6 92,0 6040 0,46
IX 75 0,485 0,447 12,6 0,302 38,2 95,9 6950 1,04
IX 76 0,465 0,433 12,5 0,256 36,2 91,5 6320 1,02
IX 77 0,400 0,384 6,9 0,232 55,4 61,3 7570 0,52
IX 78 0,443 0,422 10 0,210 50,8 83,6 7330 0,54
IX 79 0,404 0,390 7,0 0,200 35,8 55,7 5500 0,88
IX 80 0,452 0,422 10,5 0,285 36,0 82,0 6350 0,81
IX 81 0,417 0,390 9,6 0,282 35,6 98,9 6400 0,47
IX 83 0,442 0,421 8,9 0,235 54,7 62,6 8300 0,68
IX 84 0,439 0,421 7,7 0,234 63,3 71,2 6460 0,95
IX 85 0,461 0,445 7,7 0,208 55,0 62,9 7220 0,98
IX 86 0,425 0,393 10,5 0,305 36,2 94,5 6910 0,50
IX 88 0,464 0,438 10,6 0,246 35,3 91,9 7950 0,58
IX 89 0,420 0,393 9,9 0,273 43,0 87,0 5640 0,51
XII 90 0,487 0,467 8,0 0,250 69,0 79,8 6580 0,76
XII 92 0,537 0,514 8,5 0,270 34,6 70,3 4640 0,54
XII 93 0,457 0,437 8,3 0,242 55,7 63,7 7620 0,54
XII 94 0,443 0,426 8,5 0,200 58,3 77,7 6530 0,55
XII 95 0,467 0,438 9,5 0,200 43,0 70,3 6680 0,50
XII 97 0,466 0,450 7,9 0,203 53,8 73,1 6500 0,78
XII 98 0,497 0,478 8,8 0,216 54,0 87,9 7330 0,53
XII 99 0,494 0,470 8,8 0,263 50,1 65,7 6780 1,06
XII 100 0,464 0,446 8,7 0,207 35,6 65,2 6900 1,13
XII 101 0,493 0,475 8,4 0,214 38,6 69,5 7560 0,52
XII 102 0,461 0,442 8,1 0,235 66,1 81,5 8360 0,47
XII 103 0,414 0,396 7,9 0,228 44,0 76,0 6200 1,32
XII 104 0,486 0,463 8,4 0,274 46,3 61,8 6450 0,48
XII 105 0,500 0,483 8,3 0,205 42,8 86,6 6820 1,13
XII 109 0,483 0,470 5,0 0,260 42,8 78,8 8320 0,74
XII 110 0,447 0,430 7,3 0,233 50,2 89,2 6920 0,89
XII 111 0,490 0,471 7,9 0,241 42,8 87,4 7200 0,61
XII 112 0,479 0,457 8,4 0,262 60,4 67,9 7980 0,89
XIV 115 0,497 0,478 7,7 0,247 58,3 79,6 6830 0,71
XIV 116 0,478 0,462 6,9 0,232 66,1 104,9 7630 0,52
XIV 117 0,448 0,430 7,9 0,228 58,3 83,5 7000 0,49
XIV 118 0,468 0,450 7,4 0,244 35,9 88,0 6930 0,78
XIV 119 0,439 0,420 7,2 0,264 56,7 78,9 6220 1,43
XIV 121 0,482 0,468 6,8 0,206 47,5 106,8 8830 0,53
XIV 122 0,443 0,427 7,0 0,230 56,0 113,0 7120 0,49
XIV 123 0,466 0,450 7,5 0,214 32,4 73,0 7800 0,82
XIV 125 0,495 0,477 7,6 0,237 48,0 72,0 8000 0,91
XIV 126 0,445 0,430 6,9 0,218 55,1 98,3 7440 0,54
XIV 128 0,410 0,395 7,0 0,214 48,0 62,0 6120 1,32
XIV 129 0,457 0,440 7,4 0,230 39,3 47,2 7220 1,14
XIV 130 0,514 0,497 7,7 0,221 55,7 97,5 8140 0,53
XIV 132 0,505 0,487 7,8 0,230 55,7 93,5 7690 0,70
XIV 134 0,510 0,487 7,9 0,295 57,1 91,0 8000 0,70
XIV 135 0,460 0,443 6,9 0,246 31,4 63,5 7390 0,61
XIV 136 0,492 0,476 7,4 0,216 63,7 97,5 7690 0,71
XIV 137 0,499 0,482 7,8 0,218 55,4 106,8 7940 0,61
XVII 138 0,470 0,453 7,0 0,243 55,7 103,3 7550 0,61
XVII 139 0,474 0,448 8,3 0,265 47,2 96,3 7860 0,45
XVII 140 0,500 0,475 8,9 0,281 66,4 97,5 6550 0,75
XVII 141 0,525 0,503 9,3 0,237 57,4 82,0 7470 0,68
Cut Specimen Specific gravity, wet Specific gravity, dry Moisture, % Ratio \(100(\Delta_1-\Delta)/\delta\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Thickness of annual layer, mm Note
142 0,480 0,460 8,5 0,236 56,0 108,0 9500 0,43
143 0,470 0,451 8,1 0,235 56,0 94,0 8000 0,47
144 0,520 0,502 8,3 0,217 40,5 54,8 7250 0,78
145 0,458 0,440 8,5 0,212 41,2 76,3 6450 1,25
146 0,4?2 0,445 8,3 0,205 41,0 76,2 6400 1,19
148 0,483 0,450 8,1 0,284 47,5 93,0 8220 0,48
149 0,515 0,497 8,9 0,202 42,2 76,0 7150 0,89
151 0,522 0,504 8,3 0,217 64,2 86,7 7880 0,51
153 0,447 0,430 8,2 0,208 49,0 65,5 6150 1,11
154 0,467 0,449 8,0 0,225 48,6 73,7 6730 1,35
155 0,507 0,487 8,5 0,236 49,3 88,5 7350 1,25
156 0,460 0,442 8,0 0,225 55,3 121,0 7680 0,53
157 0,520 0,500 8,4 0,238 47,7 100,0 9070 0,58
158 0,523 0,503 8,8 0,227 64,0 84,0 7000 0,78
160 0,577 0,547 9,2 0,261 67,3 95,5 7770 0,84
161 0,475 0,455 7,8 0,257 41,0 94,3 8270 0,58
162 0,492 0,470 8,2 0,268 55,7 91,5 7350 0,69
163 0,545 0,523 8,8 0,250 48,0 108,0 7400 0,73
164 0,521 0,502 8,2 0,232 63,7 95,5 7940 0,66
XX 165 0,507 0,473 11,9 0,286 57,9 85,9 7450 0,64
XX 166 0,550 0,520 12,1 0,248 61,8 95,5 7000 0,61
XX 167 0,532 0,504 12,0 0,233 47,4 100,7 7720 0,83
XX 168 0,520 0,488 12,0 0,266 38,8 100,9 7690 0,54
XX 169 0,508 0,463 14,2 0,282 45,3 61,0 7090 0,95
XX 170 0,511 0,482 13,0 0,223 46,9 80,1 6460 1,06
XX 172 0,578 0,547 12,9 0,240 55,7 101,3 7940 0,48
XX 173 0,533 0,500 12,8 0,257 46,9 91,8 7750 0,63
XX 176 0,475 0,445 14,0 0,214 66,1 105,7 7890 0,74
XX 177 0,546 0,516 12,2 0,246 46,9 77,2 7450 1,25
XX 178 0,550 0,510 13,8 0,290 40,0 85,0 7680 1,16
XX 179 0,467 0,438 11,1 0,261 55,3 90,9 6950 0,89
XX 181 0,564 0,521 14,3 0,300 48,0 80,0 7110 0,98
XX 183 0,598 0,560 13,2 0,288 48,0 83,1 7450 0,64
XX 184 0,559 0,530 11,4 0,254 70,4 84,0 8090 0,81
XX 185 0,584 0,546 13,2 0,288 48,6 101,2 9200 0,78
XX 186 0,507 0,571 13,3 0,271 48,0 110,8 8170 0,64
XX 187 0,543 0,508 12,0 0,292 48,3 102,5 7450 0,64
XXI 189 0,476 0,453 10,0 0,230 46,6 93,7 8720 0,56
XXI 189 0,521 0,500 8,0 0,261 55,0 109,5 10400 0,60
XXI 190 0,544 0,536 8,4 0,214 54,1 112,0 8880 0,58
XXI 192 0,517 0,496 7,8 0,269 54,7 101,5 9030 0,94
XXI 193 0,517 0,499 8,0 0,225 47,7 86,3 7940 0,98
XXI 194 0,495 0,477 8,9 0,202 55,3 83,0 7450 1,19
XXI 195 0,529 0,505 7,9 0,304 71,2 106,8 7230 0,94
XXI 196 0,504 0,486 7,8 0,231 70,3 105,5 8470 0,64
XXI 197 0,529 0,512 8,3 0,205 73,0 112,3 8340 0,51
XXI 198 0,518 0,498 8,4 0,238 57,4 73,8 6990 0,91
XXI 199 0,446 0,431 7,2 0,208 42,6 91,5 8100 1,39
XXI 200 0,518 0,501 7,9 0,215 58,4 91,6 8280 1,19
XXI 201 0,542 0,527 9,0 0,200 95,0 129,5 7870 0,52
XXI 202 0,509 0,492 7,6 0,224 54,8 100,0 7750 0,56
XXI 203 0,531 0,512 8,0 0,238 64,0 95,3 7700 1,43
XXI 205 0,544 0,524 7,5 0,267 57,0 81,5 7560 1,19
XXI 206 0,570 0,543 9,0 0,300 62,2 106,5 9520 0,53
XXI 207 0,648 0,631 8,3 0,205 72,9 121,5 10250 0,50
XXI 211 0,578 0,553 8,5 0,294 46,6 97,0 8030 0,77
XXI 212 0,644 0,619 9,0 0,278 62,2 118,0 10100 0,82
XXI 213 0,656 0,639 6,0 0,280 78,7 128,5 8530 0,75
XXI 214 0,595 0,575 8,0 0,248 71,1 113,0 7880 0,77

Table B.

Section Sample Specific weight, wet Specific weight, dry Moisture, % Ratio \(100(\Delta_1-\Delta)/z\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² 1 scale division, mm Note
I 1 0,390 0,375 7,1 0,231 36,5 67,6 6090 0,71
I 2 0,402 0,386 7,9 0,240 53,5 69,9 6530 0,93
I 3 0,420 0,402 7,5 0,240 54,4 84,3 6150 0,98
I 4 0,410 0,392 7,7 0,233 39,0 72,3 6420 0,91
I 5 0,390 0,367 7,9 0,291 38,8 68,7 5840 0,73
I 6 0,410 0,387 8,1 0,284 41,3 82,5 7000 0,75
I 7 0,425 0,404 7,7 0,273 40,0 75,0 6860 0,88
I 8 0,425 0,407 8,4 0,215 41,3 80,4 6667 1,16
I 9 0,427 0,405 8,7 0,254 47,5 67,2 6750 1,19
I 10 0,413 0,390 8,1 0,283 31,1 77,7 6420 1,07
I 11 0,414 0,394 8,3 0,241 38,8 82,3 6340 0,77
I 13 0,398 0,386 8,3 0,241 39,2 91,9 7570 0,66
I 14 0,430 0,402 8,3 0,253 54,4 73,9 6540 0,98
I 16 0,465 0,440 9,2 0,270 39,5 74,0 7330 1,43
I 17 0,445 0,425 8,7 0,230 34,6 71,2 7280 0,63
I 18 0,403 0,385 8,0 0,225 47,8 65,4 6390 0,71
I 19 0,414 0,394 8,4 0,239 64,0 75,0 7950 0,70
I 20 0,434 0,410 8,9 0,202 38,9 76,2 7510 0,81
I 22 0,439 0,420 8,7 0,219 50,5 75,2 7320 0,84
I 24 0,389 0,363 8,5 0,306 50,7 78,1 7330 0,65
I 25 0,390 0,370 8,4 0,247 35,2 81,0 7700 0,67
III 26 0,406 0,385 8,4 0,263 46,6 70,9 7090 0,72
III 27 0,414 0,392 8,1 0,272 39,3 90,4 7210 0,93
III 28 0,423 0,402 8,2 0,266 42,7 84,5 7390 0,90
III 29 0,403 0,383 8,1 0,247 35,0 66,0 7700 0,76
III 30 0,400 0,384 7,8 0,265 42,5 63,3 7190 0,71
III 31 0,427 0,403 8,8 0,273 39,5 59,3 6950 0,88
III 32 0,438 0,416 9,0 0,243 43,7 71,6 6370 1,09
III 33 0,435 0,412 9,1 0,261 44,0 72,0 7050 1,09
III 34 0,420 0,400 8,1 0,247 40,0 78,0 6860 1,00
III 35 0,425 0,400 8,2 0,306 41,0 82,0 7310 0,69
III 37 0,420 0,397 8,3 0,277 54,4 70,0 6830 0,75
III 38 0,404 0,384 8,6 0,233 44,7 94,0 6890 0,66
III 39 0,437 0,420 8,0 0,212 39,4 79,5 6410 0,89
III 40 0,460 0,440 8,9 0,226 30,3 85,0 7350 1,35
III 41 0,475 0,450 9,2 0,272 37,8 87,1 8140 ? Knot.
III 43 0,412 0,392 7,9 0,224 47,7 81,4 7960 0,69
III 44 0,410 0,385 8,0 0,314 43,5 87,0 7560 0,73
III 45 0,440 0,418 8,5 0,259 52,0 84,0 7220 0,91
III 46 0,457 0,435 8,5 0,259 44,5 74,8 7180 1,23
III 47 0,463 0,440 9,0 0,257 49,3 82,0 7750 1,06
III 48 0,432 0,410 8,7 0,253 39,5 81,0 6950 0,73
III 49 0,445 0,422 7,8 0,192 35,3 75,0 8020 0,69
III 50 0,445 0,420 9,6 0,230 39,5 84,0 7440 0,74
III 51 0,423 0,402 8,3 0,273 48,0 84,0 6360 0,66
VI 52 0,420 0,396 9,5 0,253 40,0 86,0 6620 0,67
VI 53 0,436 0,410 9,9 0,262 38,8 80,0 6360 1,09
VI 54 0,433 0,408 9,8 0,255 45,0 83,4 6300 0,93
VI 55 0,387 0,363 8,9 0,270 33,1 61,8 7520 0,71
VI 56 0,418 0,394 10,0 0,240 38,8 69,9 6940 0,63
VI 57 0,440 0,411 10,8 0,268 39,1 70,3 6450 0,93
VI 59 0,430 0,408 10,2 0,215 38,6 78,2 6740 0,98
VI 60 0,430 0,403 10,7 0,253 40,0 72,0 7380 0,85
VI 61 0,457 0,424 12,6 0,262 40,0 60,0 6200 1,09
VI 62 0,446 0,413 11,9 0,277 39,5 68,2 6300 0,98 Slight hollows.
Section Specimen Weight, wet Weight, dry Moisture, % Ratio \(100(A_1-A)/\varphi\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Thickness of annual rings, mm Note
IX 63 0,422 0,?95 10,3 0,262 — 83,5 6400 0,74
IX 64 0,417 0,387 10,4 0,288 46,9 75,0 7050 0,67
IX 65 0,450 0,422 12,4 0,226 41,3 73,3 7000 0,93
IX 66 0,451 0,422 13,2 0,220 43,8 63,5 7330 1,35
IX 68 0,445 0,414 11,5 0,269 41,0 82,5 6950 0,85
IX 69 0,436 0,407 10,7 0,271 41,0 82,5 6900 0,71
IX 70 0,469 0,434 12,7 0,275 47,5 81,0 6830 0,88
IX 71 0,458 0,438 8,8 0,227 47,2 77,5 7610 1,39
IX 72 0,476 0,446 11,4 0,264 42,0 69,3 7070 1,06
IX 73 0,436 0,407 10,7 0,271 42,0 74,7 6940 0,74
IX 74 0,428 0,403 9,7 0,258 40,0 72,0 7870 0,70
IX 75 0,468 0,437 11,8 0,265 47,5 65,1 7330 0,85
IX 76 0,450 0,420 12,0 0,250 38,0 81,0 7540 0,88
IX 77 0,414 0,390 10,0 0,240 39,0 82,0 6900 0,72
IX 78 0,422 0,398 9,7 0,276 54,0 81,1 6780 0,82
IX 79 0,423 0,400 9,5 0,242 38,7 91,7 7450 0,86
IX 80 0,445 0,414 9,4 0,256 55,6 83,5 7110 0,81
IX 81 0,428 0,404 9,3 0,258 54,3 79,6 7390 0,79
IX 82 0,450 0,425 9,3 0,269 39,5 63,3 6750 1,00
IX 84 0,444 0,422 9,4 0,234 56,0 80,0 6770 1,04
IX 85 0,407 0,385 9,3 0,205 47,7 87,5 7320 0,75
IX 86 0,416 0,394 9,1 0,242 38,6 88,8 7210 0,69
IX 87 0,445 0,423 [[unclear: 1?,3]] 0,213 38,8 76,8 7050 0,95
IX 88 0,421 0,397 9,9 0,243 40,0 88,0 7110 0,67
IX 89 0,462 0,438 10,4 0,230 40,2 64,4 6050 1,03
IX 92 0,408 0,382 9,7 0,268 5?,3 93,6 7390 0,65
IX 93 0,464 0,435 10,3 0,282 30,8 82,5 6800 1,00
IX 96 0,449 0,422 10,2 0,265 39,5 85,0 7000 0,88
IX 97 0,433 0,414 9,8 0,194 46,7 89,4 6830 0,76
IX 99 0,445 0,414 10,4 0,260 33,8 77,0 7610 0,91
IX 100 0,48? 0,453 11,8 0,268 48,3 74,5 7730 1,39 Knot.
IX 101 0,490 0,461 10,6 0,274 47,6 81,5 79?0 1,30 Knot.
IX 102 0,473 0,447 10,7 0,248 40,0 76,8 7120 0,94
IX 103 0,422 0,395 9,? 0,273 55,3 76,0 7550 0,67
IX 104 0,414 0,392 9,0 0,244 46,6 74,6 6340 0,72
IX 105 0,466 0,435 9,9 0,232 38,8 73,8 7700 0,86
IX 106 0,452 0,428 9,7 0,248 40,0 93,0 7380 0,88
IX 107 0,420 0,396 9,2 0,261 47,7 77,6 7330 0,68
XII 108 0,426 0,406 7,6 0,263 55,7 82,7 7330 0,72
XII 110 0,446 0,422 8,2 0,293 48,3 100,0 7330 0,81
XII 111 0,436 0,412 8,2 0,293 54,0 75,3 7630 0,75
XII 112 0,470 0,448 7,7 0,286 62,7 79,0 7880 0,98
XII 113 0,465 0,445 8,0 0,250 47,3 79,1 8020 1,06
XII 114 0,470 0,448 8,4 0,262 47,4 73,6 7750 1,11
XII 116 0,412 0,390 8,4 0,262 46,6 86,3 7700 0,73
XII 117 0,410 0,390 7,9 0,253 46,6 97,5 8160 0,80
XII 119 0,466 0,444 8,2 0,268 63,9 95,0 7270 1,02
XII 120 0,428 0,410 7,9 0,228 56,0 104,0 7560 0,73
XII 121 0,402 0,382 6,9 0,289 46,6 88,3 6600 0,60
XII 122 0,457 0,440 7,0 0,242 46,6 86,5 7380 0,93
XII 123 0,473 0,455 7,2 0,250 39,5 80,0 8270 1,43
XII 125 0,408 0,383 7,8 0,256 33,8 82,5 8030 0,64
XII 126 0,432 0,413 6,9 0,276 40,0 76,4 7880 0,55
XII 127 0,488 0,466 8,5 0,259 46,6 67,7 8400 1,18
XII 128 0,495 0,477 8,0 0,225 46,6 80,7 9040 1,31
Series Specimen no. Specific gravity, wet Specific gravity, dry Moisture content % Ratio \(100(\Delta_1-\Delta)/\varphi\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Annual ring thickness, mm Note
XIV 129 0,480 0,458 8,0 0,275 46,4 82,8 8700 0,86
XIV 130 0,428 0,40 7,0 0,272 46,4 85,5 7680 0,95
XIV 131 0,408 0,392 6,7 0,239 54,3 62,2 8310 0,68
XIV 132 0,447 0,428 7,4 0,257 50,5 80,6 7810 0,80
XIV 133 0,479 0,460 7,4 0,257 56,0 88,0 8140 0,94
XIV 134 0,432 0,412 7,6 0,254 59,0 88,4 7810 0,78
XIV 135 0,479 0,460 7,6 0,250 48,2 90,4 7870 0,89
XIV 137 0,457 0,436 7,7 0,274 46,6 76,2 8380 0,82
XIV 138 0,459 0,443 7,4 0,217 51,4 77,5 7690 0,88
XIV 142 0,413 0,395 7,3 0,206 42,3 73,1 6940 0,69
XIV 146 0,415 0,415 7,2 0,278 41,5 79,9 8080 0,76
XIV 147 0,431 0,411 7,0 0,286 50,5 84,0 8400 0,62
XIV 151 0,489 0,4?0 8,2 0,232 57,1 93,7 8560 1,13
XIV 152 0,485 0,464 7,9 0,266 47,4 89,4 8220 1,00
XIV 153 0,420 0,400 7,0 0,285 39,4 108,0 7880 0,70
XIV 154 0,440 0,421 6,9 2,760 50,2 89,0 8110 0,72
XIV 156 0,490 0,467 8,0 0,288 56,0 83,0 9610 0,98
XIV 158 0,523 0,502 8,0 0,262 53,7 77,5 8300 0,96
XIV 159 0,490 0,470 6,9 0,290 55,4 91,0 7870 1,06
XIV 160 0,457 0,435 7,9 0,279 50,5 79,6 7270 0,78
XIV 161 0,420 0,390 7,7 0,285 52,0 72,0 7670 0,71
XIV 162 0,455 0,433 7,6 0,290 52,0 80,0 7870 0,85
XIV 163 0,485 0,465 7,8 0,257 52,0 90,4 8140 0,98
XIV 164 0,483 0,462 8,1 0,260 50,8 91,0 8450 1,00
XIV 165 0,463 0,442 7,8 0,269 50,2 85,0 7330 0,83
XVII 167 0,505 0,486 8,4 0,226 46,3 81,1 7540 0,65
XVII 168 0,500 0,480 8,2 0,244 54,0 85,8 7330 0,91
XVII 169 0,493 0,464 10,3 0,282 53,4 86,5 7520 0,63
XVII 166 — — — — 53,8 84,7 — —
XVII 170 0,457 0,430 9,7 0,278 53,0 73,8 6690 0,75
XVII 171 0,502 0,472 10,9 0,275 47,7 83,5 8870 0,94
XVII 173 0,486 0,453 11,2 0,294 40,0 78,0 6630 0,85
XVII 174 0,444 0,418 10,2 0,255 54,4 84,7 7390 0,76
XVII 175 0,436 0,412 9,8 0,245 40,0 82,0 7060 0,70
XVII 176 0,437 0,428 10,0 0,190 40,7 73,7 7560 1,51
XVII 181 0,525 0,500 11,3 0,221 56,7 95,2 7390 0,68
XVII 183 0,522 0,500 10,8 0,214 48,6 76,1 8180 1,32
XVII 184 0,508 0,485 11,4 0,202 47,3 77,1 7060 1,02
XVII 185 0,474 0,446 10,4 0,270 46,8 86,6 6600 0,71
XVII 186 0,448 0,428 9,5 0,210 46,8 81,6 7100 1,51
XVII 187 0,472 0,446 11,1 0,234 47,2 86,5 6700 1,25
XVII 188 0,502 0,469 11,6 0,234 46,8 83,5 8500 1,32
XVII 190 0,524 0,493 11,6 0,267 56,0 84,0 9600 1,32
XVII 191 0,513 0,480 11,7 0,283 54,4 71,8 7390 0,95
XVII 192 0,470 0,440 10,5 0,285 55,0 75,5 7050 0,73
XVII 193 0,448 0,418 10,8 0,278 54,4 79,6 7690 0,77
XVII 194 0,498 0,469 10,7 0,271 47,8 93,8 7270 0,96
XVII 195 0,527 0,504 10,0 0,230 58,4 87,7 7830 1,00
XVII 196 0,495 0,463 11,1 0,288 56,0 76,0 7750 0,91
XVII 197 0,460 0,429 10,7 0,283 55,4 76,5 7290 0,79
XX 198 0,476 0,445 10,3 0,300 46,8 77,7 6810 0,71
XX 199 0,496 0,473 10,2 0,226 53,9 77,0 7390 0,98
XX 201 0,506 0,477 10,6 0,274 46,3 79,5 7050 0,95
XX 202 0,470 0,445 9,8 0,255 54,6 87,4 7700 0,74
XX 205 0,517 0,485 11,6 0,276 46,8 67,3 9100 1,22
Section Specimen Specific gravity, wet Specific gravity, dry Moisture, % Ratio \(100(\Delta_1-\Delta)/\delta\) Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Thickness of annual rings, mm Notes
206 0,521 0,490 10,9 0,284 47,4 63,3 7270 1,06
209 0,450 0,427 10,0 0,230 61,1 83,9 7520 0,64
210 0,475 0,446 10,0 0,290 57,5 96,4 7630 0,74
211 0,463 0,438 8,4 0,298 46,8 95,2 6790 0,72
212 0,525 0,503 10,1 0,217 53,1 78,1 7730 1,06
213 0,529 0,501 11,4 0,240 47,2 76,5 8540 1,43
215 0,517 0,490 11,7 0,245 62,9 74,6 7330 1,11
216 0,530 0,506 12,0 0,246 54,0 83,4 7970 1,22
217 0,473 0,449 8,4 0,285 62,7 90,4 7590 0,81
218 0,466 0,442 9,8 0,245 45,5 95,5 7510 0,74
219 0,496 0,465 12,0 0,258 45,5 68,1 7460 1,04
220 0,534 0,505 11,7 0,248 44,6 88,9 8570 1,19
221 0,535 0,506 11,7 0,248 62,1 87,4 8880 1,25
222 0,532 0,502 11,5 0,260 63,6 79,5 7940 1,04
223 0,508 0,480 10,5 0,267 62,1 69,0 7100 0,80
224 0,456 0,431 9,6 0,261 54,4 79,7 7570 0,82
225 0,515 0,488 11,8 0,230 46,6 93,2 8030 1,16
226 0,556 0,521 11,5 0,278 44,6 90,7 7320 1,02
227 0,520 0,487 11,3 0,292 44,6 86,9 7820 1,00
228 0,485 0,460 10,1 0,247 46,6 76,9 7390 0,82
XXII 229 0,495 0,477 7,9 0,227 54,4 78,5 9220 0,78
XXII 230 0,520 0,500 8,7 0,235 56,0 80,0 8740 0,98
XXII 232 0,533 0,510 8,5 0,271 47,2 97,2 8940 1,14
XXII 233 0,507 0,485 8,8 0,250 46,6 82,4 8400 1,00
XXII 234 0,489 0,467 8,3 0,265 61,8 90,8 7640 0,78
XXII 235 0,484 0,463 7,5 0,280 44,6 77,2 3800 —
XXII 237 0,531 0,509 7,5 0,294 44,7 93,8 3660 1,16
XXII 238 0,526 0,505 7,6 0,278 55,6 112,2 8030 1,14
XXII 239 0,531 0,505 8,4 0,310 46,6 98,7 8710 1,19
XXII 240 0,509 0,487 8,6 0,256 62,5 110,0 8460 0,82
XXII 241 0,467 0,452 7,1 0,211 47,4 116,5 9260 0,70
XXII 242 0,520 0,498 8,5 0,259 70,3 114,0 8950 0,80
XXII 243 0,476 0,460 7,1 0,225 55,3 100,7 8410 0,73
XXII 244 0,570 0,544 12,2 0,262 54,1 107,0 9960 1,11
XXII 245 0,539 0,513 8,6 0,306 56,0 106,4 9150 1,43
XXII 246 0,561 0,541 8,9 0,225 63,7 97,9 9500 1,39
XXII 247 0,557 0,531 9,3 0,280 71,5 117,5 9430 1,35
XXII 248 0,534 0,518 9,3 0,226 55,3 91,0 8360 1,32
XXII 249 0,568 0,542 9,2 0,283 56,7 97,2 9470 1,14
XXII 250 0,507 0,481 8,4 0,310 56,2 98,4 7700 0,89
XXII 251 0,490 0,459 7,4 0,284 48,0 92,0 8350 0,86
XXII 252 0,512 0,497 7,0 0,214 46,6 87,5 9610 1,14
XXII 253 0,560 0,538 9,3 0,256 70,3 109,5 8610 1,25
XXII 256 0,559 0,535 9,2 0,261 54,3 84,0 9610 1,09
XXII 257 0,501 0,480 8,4 0,250 54,4 108,5 8030 1,00
XXII 258 0,480 0,458 7,8 0,282 54,4 87,5 8400 0,96
XXII 259 0,563 0,543 9,6 0,208 53,8 115,5 9470 1,06
XXII 261 0,572 0,544 9,7 0,288 55,3 82,2 9450 1,14
XXII 262 0,629 0,506 8,5 0,271 70,3 107,0 8670 1,02

Table C,

Cut Specimen No. Moisture, % Stress, wet kg/cm² Stress, dry kg/cm² Difference kg/cm² Cut Specimen No. Moisture, % Stress, wet kg/cm² Stress, dry kg/cm² Difference kg/cm²
IV 23 6,0 88,2 74,3 −13,9 XV 133 6,0 98,0 102,0 4,0
IV 24 6,5 75,0 86,7 11,7 XV 134 6,2 89,4 76,3 −13,1
IV 25 6,4 78,5 80,0 1,5 XV 135 8,5 103,3 87,6 −15,7
IV 27 6,6 75,0 65,9 −9,1 XV 136 6,1 106,7 99,2 −7,5
IV 28 6,7 79,0 69,6 −9,4 XV 138 6,2 93,8 81,5 −12,3
IV 30 6,7 80,0 89,6 9,6 XV 139 7,0 92,0 95,0 3,0
IV 31 6,3 68,9 73,7 4,8 XV 141 8,0 133,5 130,5 −3,0
IV 32 6,3 84,6 84,5 0,0 XV 142 6,1 133,5 131,5 −2,0
IV 33 7,5 82,6 81,8 −0,2 XV 143 7,1 108,0 89 −19,0
IV 35 6,2 68,5 69,3 0,8 XXI 168 5,7 114 97,7 −16,3
IV 36 6,4 80,0 94,9 14,9 XXI 169 5,5 121,5 110,0 −11,5
IV 37 7,7 82,2 80,0 −2,2 XXI 171 4,8 118,5 112,0 −6,5
IV 39 8,0 77,0 77,4 0,4 XXI 174 5,8 119,5 112,0 −7,5
IV 40 6,6 87,0 78,9 −8,1 XXI 175 5,9 94,0 88,7 −5,3
IV 41 6,4 79,8 69,7 −10,4 XXI 176 9,0 129,5 111,5 −18
IV 42 6,7 87,0 68,1 −18,9 XXI 177 5,9 86,8 87,5 0,7
IV 43 6,1 94,3 96,1 +1,8 XXI 178 9,2 129,5 108,5 −21,0
IV 44 6,6 87,0 73,3 −13,7 XXI 180 7,0 80,2 87,3 7,1
XV 119 6,1 95,6 85,6 −10,0 XXI 181 5,0 90,7 91,3 0,6
XV 121 7,0 92,3 90,0 −2,3 XXI 182 4,8 110,5 104,5 −6,0
XV 122 6,2 112,0 91,0 −21,0 XXI 183 5,9 90,7 83,3 −7,4
XV 124 6,2 83,0 70,1 −12,9 XXI 184 5,6 90,9 97,8 6,9
XV 125 6,0 110,5 100,5 −10,0 XXI 185 5,9 99,4 90,0 −9,4
XV 127 5,9 92,2 114 +21,8 XXI 188 5,0 126,1 117,3 −8,8
XV 129 6,0 85,0 93,7 8,7 XXI 189 4,9 124,2 121,5 −2,7
XV 130 6,3 110,0 101,0 −9,0 XXI 190 4,8 110,5 115,0 4,5
XV 131 7,2 102,0 91,9 −10,1

Table D.

Cut Specimen No. Moisture content % Stress, wet kg/cm² Stress, dry kg/cm² Difference kg/cm² Cut Specimen No. Moisture content % Stress, wet kg/cm² Stress, dry kg/cm² Difference kg/cm²
VII 46 8.3 76.3 78.3 2.0 96 6.7 81.6 76.3 — 5.3
VII 47 8.4 82.0 85.0 3.0 107 7.3 97.6 74.8 —22.8
VII 48 8.4 82.0 97.5 14.5 108 5.0 81.6 79.6 — 2.0
VII 49 8.5 79.6 82.5 2.9 109 7.7 86.4 75.2 —11.2
VII 50 8.3 84.7 73.3 —11.4 110 7.0 87.9 84.0 — 3.9
VII 51 8.6 80.6 79.6 — 1.0 111 6.8 86.0 75.2 —10.8
VII 53 8.0 83.5 72.6 —10.9 112 7.1 87.5 79.3 — 8.2
VII 54 7.5 78.0 74.3 — 3.7 113 7.3 98.3 82.0 —16.3
VII 55 8.2 96.6 92.7 — 3.9 114 7.6 80.1 72.2 — 7.9
VII 56 7.9 108.0 99.1 — 8.9 XVIII 166 6.7 86.0 77.0 — 9.0
VII 57 7.9 101.2 92.4 — 8.8 XVIII 167 7.0 99.5 94.0 — 5.5
VII 58 7.0 87.0 86.7 — 0.3 XVIII 168 7.0 92.3 82.0 —10.3
VII 59 6.8 87.4 71.2 —16.2 XVIII 169 6.9 84.5 77.9 — 6.6
VII 60 7.2 81.0 72.7 — 8.3 XVIII 170 7.0 87.0 79.0 — 8.0
VII 62 7.6 89.5 81.5 — 8.0 XVIII 171 6.8 85.4 68.0 —17.4
VII 63 7.5 92.7 71.0 —21.7 XVIII 172 7.0 86.0 82.0 — 4.0
VII 64 7.8 83.5 82.5 — 1.0 XVIII 173 7.0 92.1 79.3 —12.8
VII 65 7.8 82.5 71.7 —10.8 XVIII 174 7.0 85.0 67.6 —17.4
VII 66 7.4 101.0 88.2 —12.8 XVIII 175 6.5 96.3 88.7 — 7.6
VII 67 7.9 108.0 93.4 —14.6 XVIII 177 7.0 101.5 94.4 — 7.1
VII 68 6.5 90.0 66.4 —23.6 XVIII 178 6.9 94.0 94.8 0.8
XI 92 6.7 93.5 80.0 —13.5 XVIII 179 7.0 89.9 78.8 —11.1
XI 94 6.5 89.5 98.4 — 8.9 XVIII 180 7.1 93.8 77.3 —16.5
XI 95 6.0 89.6 88.6 7.0 XVIII 183 7.0 90.0 79.3 —10.7
XI 98 7.3 80.0 69.3 —10.7 XVIII 184 6.4 90.5 82.5 — 8.0
XI 99 7.5 91.0 78.4 —12.6 XVIII 185 6.5 106.0 98.4 — 7.6
XI 100 5.0 90.2 91.2 1.0 XVIII 186 6.1 107.3 74.2 —33.1
XI 102 7.6 89.9 82.0 — 7.9 XVIII 187 6.0 88.0 83.0 — 5.0
XI 103 5.0 87.9 90.2 2.3 XVIII 189 6.0 91.5 86.0 — 5.5
XI 104 6.7 88.0 81.3 — 6.7 XVIII 190 5.7 101.5 103.0 1.5
XI 105 7.2 87.4 79.3 — 8.1 XVIII 191 6.3 106.6 97.2 — 9.4
XI 106 7.3 77.0 72.6 — 4.4 XVIII 192 5.6 83.0 79.0 — 4.0

Table E.

Specimen Sample No. Moisture, % Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Specimen Sample No. Moisture, % Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm²
V 1 7,7 317 458 63400 XVI 47 5,5 557 635 74600
V 2 7,6 286 486 71800 XVI 48 5,5 545 643 73300
V 3 7,6 283 468 73200 XVI 49 5,4 370 622 74500
V 4 7,8 363 520 10800 XVI 50 5,7 343 628 81000
V 5 7,5 420 465 73200 XVI 51 5,6 379 706 95000
V 7 7,4 347 463 68300 XVI 54 5,6 433 620 7400
V 8 7,7 358 463 74500 XVI 55 5,7 433 632 83100
V 10 7,2 375 490 61000 XVI 56 5,2 552 703 97000
V 11 7,6 380 476 67200 XVI 57 5,3 514 687 101000
V 12 6,6 353 463 80000 XVI 58 5,6 406 660 85200
V 13 6,9 321 561 95300 XVI 61 5,0 473 627 96800
V 14 7,2 358 500 66300 XVI 62 5,1 393 604 90200
V 17 7,3 368 498 74700 XVI 63 5,4 225 496 78000
V 18 6,8 319 543 76200 XVI 64 5,4 513 573 88500
V 19 7,2 333 414 52500 XVI 65 4,8 348 682 103000
V 20 7,5 343 512 61300 XVI 67 4,9 437 750 109000
V 21 7,4 400 540 [[unclear: 5?300]] XVI 68 5,0 428 575 74300
VIII 2 7,6 386 422 65800 XVI 69 5,1 319 614 94500
VIII 23 6,9 373 374 56500 XVI 70 5,3 406 655 99300
VIII 24 7,6 314 511 71400 XVI 71 5,5 433 688 97000
VIII 25 7,6 347 514 81000 XIX 72 5,4 263 646 107000
VIII 26 5,8 232 426 — XIX 73 5,3 467 688 97500
VIII 27 6,0 334 500 76000 XIX 74 5,4 346 [[unclear: 6?8]] 84700
VIII 28 7,0 350 531 72000 XIX 75 5,3 493 664 76300
VIII 31 6,8 349 577 75500 XIX 76 5,2 293 707 97700
VIII 33 7,1 375 538 77700 XIX 77 5,5 430 666 95600
VIII 34 7,1 256 353 48000 XIX 79 5,5 235 530 98000
VIII 35 5,7 437 575 94000 XIX 80 5,2 340 600 96000
VIII 36 5,8 383 625 94600 XIX 82 5,3 347 692 103500
VIII 37 5,4 347 570 67200 XIX 83 5,2 461 550 74500
VIII 38 6,0 334 468 76000 XIX 85 5,4 263 768 101000
VIII 40 5,6 364 564 100000 XIX 86 5,4 373 620 74200
VIII 41 6,2 345 493 72700 XIX 87 5,0 340 700 95000
VIII 42 6,4 350 483 50800 XIX 88 5,4 616 792 107000
VIII 43 7,0 314 431 48700 XIX 90 5,4 407 743 90000
VIII 44 7,1 314 517 68200 XIX 92 5,4 399 713 100000
XVI 45 7,0 314 472 64000 XIX 93 5,7 374 718 10500
XVI 46 5,8 403 581 83300 XIX 94 5,4 250 644 121000

Table F.

Series Sample No. Moisture, % Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm² Series Sample No. Moisture, % Stress \(K_1\), kg/cm² Stress \(K_2\), kg/cm² Modulus of elasticity, kg/cm²
V 1 5.1 374 465 58300 XVI 66 7.0 278 500 87000
V 2 6.0 407 486 58600 XVI 69 7.0 281 490 77000
V 3 5.7 409 532 66700 XVI 70 6.4 361 508 68000
V 4 6.4 313 437 55300 XVI 72 6.8 397 610 93500
V 5 9.3 316 452 54300 XVI 73 7.2 376 595 96000
V 6 6.9 313 523 85000 XVI 74 6.7 307 602 94500
V 7 6.7 397 533 70400 XVI 75 7.0 340 600 88200
V 8 7.0 463 512 76600 XVI 76 7.0 286 530 91000
V 9 6.8 318 448 69500 XVI 77 7.0 2 4 512 76500
V 12 7.1 233 460 57700 XVI 78 6.5 346 590 85500
V 13 7.1 360 460 47000 XVI 79 6.9 292 623 82300
V 14 6.5 491 563 82000 XVI 81 7.0 290 587 71500
V 18 6.8 316 492 69500 XVI 82 4.5 398 613 81200
V 19 6.3 323 538 83700 XVI 83 7.0 350 545 72300
V 21 6.3 508 630 85400 XVI 84 6.2 288 323 96000
V 22 6.8 290 517 87000 XVI 85 6.1 387 633 99200
V 23 7.0 258 442 76500 XVI 86 5.9 314 654 94700
V 24 7.1 381 548 80500 XVI 87 6.3 234 604 139000
V 25 7.6 295 568 86600 XVI 88 6.0 410 565 86500
V 26 6.1 381 488 71400 XIX 89 5.5 289 508 70500
VIII 27 5.8 324 476 60200 XIX 90 5.3 423 635 94500
VIII 28 5.7 256 522 78000 XIX 91 5.8 423 667 105000
VIII 29 5.7 312 515 73800 XIX 92 6.4 420 625 90200
VIII 30 5.9 249 510 83000 XIX 93 6.3 273 530 74000
VIII 31 5.8 412 580 87600 XIX 94 6.5 342 536 86700
VIII 32 5.9 400 550 74300 XIX 96 6.2 440 610 114000
VIII 33 6.3 433 560 74500 XIX 97 6.0 363 650 124000
VIII 35 5.8 316 468 63500 XIX 98 6.1 317 613 85600
VIII 36 5.8 372 557 93000 XIX 99 6.5 309 530 90500
VIII 41 5.8 286 437 71300 XIX 100 6.4 276 520 71000
VIII 42 5.5 354 546 75500 XIX 101 6.7 314 535 79000
VIII 46 5.5 367 512 73300 XIX 102 6.5 337 536 83000
VIII 47 5.6 314 482 73100 XIX 103 6.3 284 636 113500
VIII 49 6.1 403 538 62500 XIX 104 6.6 358 635 103500
VIII 50 5.7 518 642 87000 XIX 105 7.0 292 635 122000
VIII 51 6.1 265 515 89000 XIX 106 6.7 407 645 118000
VIII 52 5.4 352 482 59000 XIX 107 6.3 368 648 141500
VIII 53 5.5 378 507 58200 XIX 108 6.7 286 580 114500
VIII 54 5.8 496 600 73000 XIX 109 6.3 279 560 90300
VIII 55 5.2 407 593 94000 XIX 110 6.6 286 627 124000
VIII 56 5.9 290 507 78700 XIX 111 6.5 3 3 645 102000
XVI 57 5.4 306 517 73800 XIX 112 8.2 276 645 103000
XVI 58 5.7 414 565 82700 XIX 113 6.6 282 660 125500
XVI 59 6.3 354 567 87000 XIX 114 6.6 330 567 103000
XVI 60 6.9 318 573 81500 XIX 115 6.4 283 545 105000
XVI 61 6.9 310 505 72900 XIX 116 6.6 255 625 84000
XVI 62 6.8 431 580 85500 XIX 117 7.2 494 647 88000
XVI 64 6.4 541 568 115000 XIX 118 6.9 475 610 104000
XVI 65 6.7 345 515 72000 XIX 119 7.2 298 557 112000

Table G.

Batch Specimen No. Moisture, % Specific weight Stress, kg/cm² Batch Specimen No. Moisture, % Specific weight Stress, kg/cm²
II 2 6,1 0,368 99,0 XXI 197 7,4 0,405 109,0
II 3 6,8 0,388 92,7 XXI 198 7,5 0,480 107,0
II 4 6,2 0,365 83,0 XXI 199 7,5 0,460 120,0
II 5 7,1 0,344 94,6 XXI 200 7,4 0,463 116,0
II 6 6,6 0,384 99,0 XXI 201 8,4 0,473 111,3
II 7 7,6 0,407 93,7 XXI 202 7,3 0,460 103,0
II 8 — — 92,0 XXI 204 7,9 0,490 117,0
II 9 7,3 0,393 84,7 XXI 205 7,0 0,422 95,5
II 11 6,4 0,395 90,3 XXI 206 7,6 0,490 117,3
II 12 6,7 0,407 89,7 XXI 207 6,9 0,480 109,3
II 13 8,0 0,437 86,3 XXI 208 7,7 0,475 108,3
II 14 7,5 0,446 103,0 XXI 209 8,8 0,490 128,0
II 15 6,8 0,412 96,3 XXI 210 8,4 0,480 103,0
II 16 — — 91,3 XXI 211 8,0 0,430 102,7
II 17 5,7 0,395 93,0 XXI 212 8,3 0,440 96,7
II 18 6,6 0,398 98,7 XXI 214 8,4 0,470 105,7
II 19 6,7 0,379 85,0 XXI 215 8,5 0,493 104,3
II 20 6,5 0,418 85,0 XXI 216 8,6 0,485 106,3
II 21 6,5 0,400 83,8 XXI 217 7,9 0,520 128,0
II 22 7,0 0,355 91,0 XXI 218 7,9 0,480 110,0
XXI 193 7,1 0,500 94,0 XXI 219 8,3 0,485 105,3
XXI 194 6,9 0,465 95,7 XXI 220 8,8 0,520 113,0
XXI 195 7,8 0,507 100,0 XXI 221 8,6 0,492 122,0
XXI 196 7,4 0,452 98,3 XXI 222 8,3 0,430 109,0

Corrected Misprints:

Page Line Printed: Should read:
1 13 from below Jank’a Janka
3 3 from top Fay ’Tay
11 16 from below $\lambda,=\Delta A(\varphi-10)$ $\lambda,=\Delta-A(\varphi-10)$
12 9 from below oscillations oscillation
12 16 from top steps degrees
13 2 from below 1.6 klg/cm 1.6 kg/cm²
16 Table VIII $g:k_2$ $G:k_2$
  1. The Institution of Mech. Eng. 1906. ↩

  2. Philosoph. Transactions of the royal Society 1829. ↩

  3. According to Burr’s The elasticity and resistance of the material engineering. ↩

  4. Résistance des bois à la torsion. ↩

  5. \(\Delta\) has been increased 100-fold. ↩

  6. We consider it necessary to recall that by completely dry wood we mean wood dried at approximately \(100^\circ\) C. ↩

Submission history

On the Problem of the Shear Resistance of Wood