Approximate solution of elastoplastic problems in the theory of ideal plasticity
Unknown
Submitted 1957-01-01 | SovietRxiv: ru-195701.12059 | Translated from Russian

Abstract Generated abstract

This paper develops a perturbation method for approximate elastoplastic solutions in ideal plasticity, expanding stresses and unknown boundaries in powers of a small parameter. For plane strain and plane stress, it derives successive conditions from the Mises and Saint-Venant yield criteria, linearized boundary conditions, and matching conditions at the elastic-plastic interface. The method is then applied to several problems involving plates with circular or elliptical holes under biaxial tension and an eccentric tube under internal pressure. The resulting series give approximations to the plastic-zone boundary, including a case where the expansion agrees with the known exact elliptical solution.

Full Text

THEORY OF ELASTICITY

D. D. IVLEV

APPROXIMATE SOLUTION OF ELASTOPLASTIC PROBLEMS OF THE THEORY OF IDEAL PLASTICITY

(Presented by Academician A. I. Nekrasov, 12 X 1956)

We shall seek the solution of the elastoplastic problem in the form of series in powers of a certain parameter \(\delta\):

\[ \sigma_{ij}=\sum_{n=0}\delta^n\sigma_{ij}^{(n)},\qquad \sigma_{ii}\equiv\sigma_\rho,\qquad \sigma_{jj}\equiv\sigma_\theta,\qquad \sigma_{ij}\equiv\sigma_{ji}\equiv\tau_{\rho\theta}. \tag{1} \]

We shall confine ourselves to consideration, in the theory of plane strain, of the plasticity conditions of Mises and Saint-Venant \((^1)\), which are essentially coincident:

\[ \frac14(\sigma_\rho-\sigma_\theta)^2+\tau_{\rho\theta}^2=1; \tag{2} \]

in the theory of plane stress—the Saint-Venant plasticity condition \((^1)\):

\[ \frac14(\sigma-\sigma_\theta)^2+\tau_{\rho\theta}^2= \left[1-\frac12(\sigma_\rho+\sigma_\theta)\right]^2 \quad \text{for } \sigma_\theta>\sigma_\rho>0. \tag{3} \]

In (1), (2), (3) all quantities are dimensionless. Substituting (1) into (2), with \(\tau_{\rho\theta}^0=0\), we obtain:

\[ \sigma_\rho'-\sigma_\theta'=0,\qquad (\sigma_\rho''-\sigma_\theta'')\mu+\tau_{\rho\theta}'^{\,2}=0,\qquad \frac12(\sigma_\rho'''-\sigma_\theta''')\mu+\tau_{\rho\theta}'\tau_{\rho\theta}''=0, \tag{4} \]

where \(\mu=\operatorname{sign}(\sigma_\rho^0-\sigma_\theta^0)\).

Substituting (1) into (3) with \(\tau_{\rho\theta}^0=0\), we obtain:

\[ \sigma_\theta'=0,\qquad (1-\sigma_\rho^0)\sigma_\theta''+\tau_{\rho\theta}'^{\,2}=0,\qquad (1-\sigma_\rho^0)\sigma_\theta'''-\sigma_\rho'\sigma_\theta''+2\tau_{\rho\theta}'\tau_{\rho\theta}''=0. \tag{5} \]

If on the boundary \(L\) of the body under consideration

\[ \sigma_{\mathrm n}=P_{\mathrm n},\qquad \tau_{\mathrm n}=P_\tau, \tag{6} \]

then, assuming the equation of the contour \(L\) to be given in the form

\[ \rho=\sum_{n=0}\delta^n\rho_n(\theta), \]

we obtain the linearized boundary conditions (6) in the form

\[ \sigma_\rho' + \frac{d\sigma_\rho^0}{d\rho}\rho_1 = \frac{dP_{\mathrm n}}{d\rho}\rho_1;\qquad \tau_{\rho\theta}'-(\sigma_\theta^0-\sigma_\rho^0)\dot R_1 = \frac{dP_\tau}{d\rho}\rho_1; \]

\[ \sigma_\rho''+ \frac{d\sigma_\rho'}{d\rho}\rho_1+ \frac{d^2\sigma_\rho^0}{d\rho^2}\frac{\rho_1^2}{2!} + \frac{d\sigma_\rho^0}{d\rho}\rho_2 + (\sigma_\theta^0-\sigma_\rho^0)\dot R_1^{\,2} - 2\tau_{\rho\theta}'\dot R_1 = \]

\[ = \frac{d^2P_{\mathrm n}}{d\rho^2}\frac{\rho_1^2}{2!} + \frac{dP_{\mathrm n}}{d\rho}\rho_2; \]

\[ \begin{gathered} \tau_{\rho\theta}^{\prime\prime} -(\sigma_\theta^0-\sigma_\rho^0)(\dot R_2-R_1\dot R_1) -(\sigma_\theta'-\sigma_\rho')\dot R_1 +\frac{d}{d\rho}\left[\tau_{\rho\theta}'-(\sigma_\theta^0-\sigma_\rho^0)\dot R_1\right]\rho_1 =\\ =\frac{d^2P_\tau}{d\rho^2}\frac{\rho_1^2}{2!} +\frac{dP_\tau}{d\rho}\rho_2; \end{gathered} \tag{7} \]

\[ \begin{gathered} \sigma_\rho^{\prime\prime\prime} +\frac{d\sigma_\rho^{\prime\prime}}{d\rho}\rho_1 +\frac{d^2\sigma_\rho'}{d\rho^2}\frac{\rho_1^2}{2!} +\frac{d^3\sigma_\rho^0}{d\rho^3}\frac{\rho_1^3}{3!} +2(\sigma_\theta^0-\sigma_\rho^0)(\dot R_1\dot R_2-R_1\dot R_1^2)+\\ +\frac{d(\sigma_\theta-\sigma_\rho)}{d\rho}\dot R_1^2\rho_1 -(\sigma_\theta'-\sigma_\rho')\dot R_1^2 -2\tau_{\rho\theta}'(\dot R_2-R_1\dot R_1)-\\ -2\frac{d\tau_{\rho\theta}}{d\rho}\dot R_1\rho_1 -2\tau_{\rho\theta}^{\prime\prime}\dot R_1 +\frac{d\sigma_\rho'}{d\rho}\rho_2 +\frac{d^2\sigma_\rho^0}{d\rho^2}\rho_1\rho_2 +\frac{d\sigma_\rho^0}{d\rho}\rho_3=\\ =\frac{d^3P_\Pi}{d\rho^3}\frac{\rho_1^3}{3!} +\frac{d^2P_\Pi}{d\rho^2}\rho_1\rho_2 +\frac{dP_\Pi}{d\rho}\rho_3; \end{gathered} \]

\[ \begin{gathered} \tau_{\rho\theta}^{\prime\prime\prime} -2\tau_{\rho\theta}'\dot R_1^2 -(\sigma_\theta^0-\sigma_\rho^0)(\dot R_3-R_1\dot R_2+R_1^2\dot R_1-\dot R_1R_2-\dot R_1^3)-\\ -(\sigma_\theta'-\sigma_\rho')(\dot R_2-R_1\dot R_1) -(\sigma_\theta^{\prime\prime}-\sigma_\rho^{\prime\prime})\dot R_1 +\frac{d}{d\rho}\left[\tau_{\rho\theta}^{\prime\prime}-(\sigma_\theta^0-\sigma_\rho^0)(\dot R_2-R_1\dot R_1)-\right.\\ \left.-(\sigma_\theta'-\sigma_\rho')\dot R_1\right]\rho_1 +\frac{d^2}{d\rho^2}\left[\tau_{\rho\theta}'-(\sigma_\theta^0-\sigma_\rho^0)\dot R_1\right]\frac{\rho_1^2}{2!} +\frac{d}{d\rho}\left[\tau_{\rho\theta}'-(\sigma_\theta^0-\sigma_\rho^0)\dot R_1\right]\rho_2=\\ =\frac{d^3P_\tau}{d\rho^3}\frac{\rho_1^3}{3!} +\frac{d^2P_\tau}{d\rho^2}\rho_1\rho_2 +\frac{dP_\tau}{d\rho}\rho_3, \end{gathered} \]

where \(R_i=\rho_i/\rho_0\).

Since on the boundary of the plastic region \(L_s\) the solutions for the plastic and elastic regions are matched continuously (1):

\[ [\sigma_\rho]=[\sigma_\theta]=[\tau_{\rho\theta}]=0 \quad \text{on } L_s, \tag{8} \]

then, representing the equation of the contour \(L_s\) in the form

\[ \rho_s=\sum_{n=0}\delta^n\rho_{sn}(\theta), \tag{9} \]

we obtain the linearized matching conditions (8) in the form

\[ \begin{gathered} \left[\sigma_{ij}'+\frac{d\sigma_{ij}^0}{d\rho}\rho_{s1}\right]=0,\qquad \left[\sigma_{ij}^{\prime\prime} +\frac{d\sigma_{ij}'}{d\rho}\rho_{s1} +\frac{d^2\sigma_{ij}^0}{d\rho^2}\frac{\rho_{s1}^2}{2!} +\frac{d\sigma_{ij}^0}{d\rho}\rho_{s2}\right]=0;\\ \left[\sigma_{ij}^{\prime\prime\prime} +\frac{d\sigma_{ij}^{\prime\prime}}{d\rho}\rho_{s1} +\frac{d^2\sigma_{ij}'}{d\rho^2}\frac{\rho_{s1}^2}{2!} +\frac{d^3\sigma_{ij}^0}{d\rho^3}\frac{\rho_{s1}^3}{3!} +\frac{d\sigma_{ij}^0}{d\rho}\rho_{s3} +\frac{d\sigma_{ij}'}{d\rho}\rho_{s2}+\right. \tag{10}\\ \left. +\frac{d^2\sigma_{ij}^0}{d\rho^2}\rho_{s1}\rho_{s2} \right]=0\ \text{etc.} \end{gathered} \]

We note that from the equilibrium equations and conditions (8) it follows that

\[ \left[\frac{d\sigma_\rho^0}{d\rho}\right]=0 \quad \text{on } L_s . \]

Consequently, the matching conditions (10) for \(\sigma_\rho\) and \(\tau^{\rho\theta}\) play the role of boundary conditions for determining the stresses in the elastic region, while the matching condition for \(\sigma_\theta\) serves to determine \(\rho_{sn}\). The greatest difficulty and interest in such problems is the determination of the equation of the boundary of the plastic zone \(L_s\). We shall present several approximate solutions.

  1. Biaxial tension of a thick plate with a circular hole of radius \(a\) by forces \(P_1\) and \(P_2\). Denoting

\[ \delta=\frac{|P_1-P_2|}{2k}, \tag{11} \]

where \(k=\frac14\sigma_s\) according to Saint-Venant and \(k=\frac13\sigma_s\) according to Mises, one may obtain:

\[ \rho_s=1+\delta\cos 2\theta-\frac34\delta^2(1-\cos 4\theta)+\frac58\delta^3(-\cos 2\theta+\cos 6\theta)+ \]
\[ +\frac{7}{64}\delta^4(-1-4\cos 4\theta+5\cos 8\theta)+\cdots \tag{12} \]

Expansion (12) coincides exactly with the expansion of the equation of an ellipse with semiaxes \((1+\delta)\), \((1-\delta)\), which, as shown in \((^2)\), is the exact solution of this problem.

  1. Biaxial tension of a thin plate with a circular hole of radius \(a\) by forces \(P_1\) and \(P_2\). Introducing \(\delta\) (11), one may obtain:

\[ \rho_s=1+4\delta^*\cos 2\theta-8\delta^{*2}(1-2\cos 4\theta)-80\delta^{*3}(\cos 2\theta-\cos 6\theta)+ \]
\[ +32\delta^{*4}(1-16\cos 4\theta+14\cos 8\theta)+\cdots, \tag{13} \]

where \(\delta^*=\delta/\alpha;\ \alpha=a/r_s^0;\ r_s^0\) is the size of the radius of the plastic zone for \(\delta=0\). The first approximation (13) was obtained in \((^3)\).

  1. Biaxial tension of a thin plate with an elliptical hole by forces \(P_1d_2\) and \(P_2d_2\), directed at an angle \(\theta_0\) to the principal central axes of the ellipse. Introducing \(\delta\) (11), one may obtain:

\[ \rho_s=1+\delta^*(4d_2\cos 2(\theta-\theta_0)+3\alpha d_1\cos 2\theta)+\delta^{*2}\{d_1^2(\alpha^2/4-8\alpha^4)- \]
\[ -(18d_1d_2\alpha\cos 2\theta_0+8d_2^2)+[-d_1^2(15/4\,\alpha^2-8\alpha^3-3/4\,\alpha^4)+ \]
\[ +(18d_1d_2\alpha\cos 2\theta_0+16d_2^2\cos 4\theta_0)]\cos 4\theta+ \]
\[ +[18d_1d_2\alpha\sin 2\theta_0+16d_2^2\sin 4\theta_0]\sin 4\theta\}+\cdots, \]

where the equation of the ellipse of the hole is represented in the form

\[ \rho=\alpha+\delta\alpha d_1\cos 2\theta-\delta^2\frac{3\alpha d_1^2}{4}(1-\cos 4\theta)+\cdots . \]

For \(d_1=0,\ \theta_0=0,\ d_2=1\) there is the case of biaxial tension of a thin plate with a circular hole; for \(d_2=0,\ d_1=1\), the case of uniform tension of a thin plate with an elliptical hole.

  1. An eccentric tube under the action of internal pressure \(p_0\). Referring all linear quantities to the outer radius of the tube \(b\), denote \(\delta=c/b\), where \(c\) is the eccentricity of the tube. One may obtain:

\[ \rho_s=\beta_0-\delta\frac{2\beta_0^4}{1-\beta_0^4}\cos\theta+\delta^2\left\{\frac{\beta_0^3(2-\beta_0^4-\beta_0^6)}{(1-\beta_0^2)(1-\beta_0^4)^2}+\frac{2\beta_0^7}{(1-\beta_0^4)^2}+\right. \]
\[ +\frac{1}{N}\left[-\frac{(1-\beta_0^2)(1-3\beta_0^4)}{\beta_0} +\frac{(1-\beta_0^2)^2(5+3\beta_0^4)\beta_0}{(1-\beta_0^4)}-\right. \]
\[ \left.\left.-\frac{\beta_0^3}{(1-\beta_0^4)^2}\bigl[(1+\beta_0^2)^4+4\beta_0^4(2-\beta_0^2)^2-4(1+4\beta_0^4)\bigr] +\frac{2\beta_0^3(1-\beta_0^2)^2}{(1+\beta_0^2)^2}\right]\cos 2\theta\right\}, \]

where \(\beta_0=r_s^0/b,\ N=(\beta_0-1/\beta_0)^4\).

Moscow State University
named after M. V. Lomonosov

Received
9 X 1956

References

  1. V. V. Sokolovskii, Theory of Plasticity, Moscow, 1950.
  2. L. A. Galin, Applied Mathematics and Mechanics, vol. 3 (1946).
  3. A. P. Sokolov, DAN, vol. 60, No. 1 (1948).
  4. G. N. Savin, Stress Concentration around Holes, Moscow, 1951.

Submission history

Approximate solution of elastoplastic problems in the theory of ideal plasticity