1. |
Optimum design of composite laminates with STROPT |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 863-871
S. Belsare,
M. Haririan,
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摘要:
AbstractThe design of a composite laminate involves the determination of layer thicknesses and orientation angles. The problem is posed as the optimum weight (or volume) design of composite laminates which withstand the specified loads without failure. The modified Hill‐Mises or Tsai‐Wu failure criterion is taken as a constraint, each layer being subjected to this criterion. The design variables considered are the layer thicknesses and orientation angles. Based on the finite‐element analysis capability of composite laminates provided by NISA II, a composite laminate optimization procedure has been developed. Nonlinear optimization techniques are used to approach the optimum design of the composite laminates. Efficient design sensitivity analysis procedures are implemented based on the direct differentiation and adjoint variable methods. Example problems illustrate that the program offers an efficient and practical design tool for composite lami
ISSN:1069-8299
DOI:10.1002/cnm.1640091102
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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2. |
A simple time‐step control scheme |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 873-881
Dan Givoli,
Ilan Henigsberg,
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摘要:
AbstractA simple automatic time‐step control procedure is devised for use in implicit one‐step time‐integration schemes. First‐ and second‐order semi‐discrete systems of equations emanating from finite‐element spatial discretization are considered. The varying time‐step interval is controlled by the relative distance between the solution in two consecutive time steps, using the solution update formula of the time integrator under consideration. A model problem involving the vibrations of a membrane is used to demonstrate the performanc
ISSN:1069-8299
DOI:10.1002/cnm.1640091103
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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3. |
Finite‐element analysis of elastic contact between a shell of revolution and a rigid plate |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 883-888
B. P. Gautham,
N. Ganesan,
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摘要:
AbstractElastic contact between a thick shell of revolution and a rigid plate in the case when the plate is brought into contact with the shell by giving a finite displacement to the plate is analysed by the finite‐element method. Field‐consistent higher‐order strain‐displacement relations with vanishing shear stresses on the surfaces are used. A finite element based on these relations is developed and used for the analysis. The contact conditions are imposed by use of the Lagrangian multipliers method, and the resulting minimization problem is solved iteratively. This procedure will lead to reduced memory requirements and computati
ISSN:1069-8299
DOI:10.1002/cnm.1640091104
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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4. |
Computation of isotropic tensor functions |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 889-896
C. Miehe,
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摘要:
AbstractAn explicit formulation and a procedure for the computation of isotropic tensor‐valued tensor functions is discussed. The formulation is based on a spectral decomposition in terms of second‐order eigenvalue bases, which avoids the costly computation of eigenvectors. As an important result a compact structure of the fourth‐order derivatives of general second‐order isotropic tensor functions is pr
ISSN:1069-8299
DOI:10.1002/cnm.1640091105
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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5. |
Use of load‐dependent vectors for dynamic analysis of large space structures |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 897-908
J. M. Ricles,
P. Léger,
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摘要:
AbstractStructural models of large space structures have a substantial number of degrees of freedom (DOF) and possess semi‐positive‐definite stiffness matrices. The paper presents an efficient co‐ordinate reduction procedure for structural dynamic analysis of large space structures. The method is based on the superposition of load‐dependent Ritz vectors, which are computed in block form using a shifted stiffness matrix. Comparative transient dynamic analyses are performed on a 2803 DOF model of the space station Freedom using the load‐dependent method (LDM) and the mode‐displacement method (MDM) based on the superposition of eigenvectors. It is shown that the LDM is able to provide convergence of displacements with a small number of vectors. The acceleration response is found to be more sensitive to vector truncation than the displacement response. Error norms based on the representation of the dynamic load by the vector basis are developed to provide an indication of the effect of vector truncation on the structur
ISSN:1069-8299
DOI:10.1002/cnm.1640091106
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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6. |
Analytic evaluation of singular boundary integrals without CPV |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 909-915
Earlin D. Lutz,
L. J. Gray,
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摘要:
AbstractBoundary integral equations are generally derived by employing a Cauchy Principal Value definition for the singular integral involving the derivative of the Green function. As a consequence, evaluation of this integral requires special attention, and computing the associated ‘solid angle coefficient’ can often pose difficulties. As discussed herein, these problems can be avoided by defining the integral directly, in terms of a limit to the boundary. This approach leads to a straightforward evaluation proced
ISSN:1069-8299
DOI:10.1002/cnm.1640091107
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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7. |
BEM analysis of reduced dynamic stress concentration by multiple holes |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 917-924
C. P. Providakis,
D. A. Sotiropoulos,
D. E. Beskos,
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摘要:
AbstractThe reduction of stress concentration around a circular hole in a dynamically loaded plate by introducing auxiliary holes around the original hole is studied numerically. The solution of this plane stress problem is carried out in the Laplace transformed domain with the aid of the boundary‐element method, and subsequently the time domain response is obtained by numerically inverting the transformed solution. Numerical examples are presented which demonstrate a stress reduction as high as 18 per pent by the introduction of two auxiliary holes in the loading direction for the uniaxial cas
ISSN:1069-8299
DOI:10.1002/cnm.1640091108
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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8. |
Comparison of strain recovery techniques for the mixed iterative method |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 925-932
Jan Červenka,
Scott C. Keating,
Carlos A. Felippa,
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摘要:
AbstractThree strain recovery techniques are investigated in the framework of the mixed iterative method. The need for appropriate strain recovery for low‐order elements is shown. The three techniques compared are: C‐lumping, strain‐smoothing and a new technique called C‐splitting. It is shown that the use of C‐lumping has negative effects on the convergence of the mixed iterative method. Both strain‐smoothing and C‐splitting deliver convergent results, but the new technique con
ISSN:1069-8299
DOI:10.1002/cnm.1640091109
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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9. |
Conference diary |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page 933-935
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ISSN:1069-8299
DOI:10.1002/cnm.1640091110
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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10. |
Masthead |
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Communications in Numerical Methods in Engineering,
Volume 9,
Issue 11,
1993,
Page -
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PDF (111KB)
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ISSN:1069-8299
DOI:10.1002/cnm.1640091101
出版商:John Wiley&Sons, Ltd
年代:1993
数据来源: WILEY
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