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‡a(MiU)99187539618706381
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‡asdr-miu.99187539618706381
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‡aD 301.45/46-2:68-39
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‡aAD 0708516
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‡aAFFDL TR 68-39
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100 |
1 |
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‡aSalmon, M.,
‡eauthor.
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‡aAn application of the finite element method to elastic-plastic problems of plane stress /
‡cby M. Salmon, L. Berke and R. Sandhu.
|
264 |
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1 |
‡aWright-Patterson Air Force Base, Ohio :
‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force,
‡c1970.
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300 |
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‡avi, 48 pages :
‡billustrations, figures, tables ;
‡c28 cm.
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336 |
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‡atext
‡btxt
‡2rdacontent
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337 |
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‡aunmediated
‡bn
‡2rdamedia
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‡avolume
‡bnc
‡2rdacarrier
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‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ;
‡vAFFDL TR 68-39
|
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‡aAD0708516 (from http://www.dtic.mil).
|
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‡a"This report was prepared by the Illinois Institute of Technology Research Institute and The Air Force Flight Dynamics Laboratory as a joint in-house effort under Project No. 1467."
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‡a"IIT Research Institute. Chicago, Illinois."
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‡a"May 1970."
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‡aIncludes bibliographical references (page 29).
|
520 |
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‡aA computer program is presented for the small strain analysis of plane structures in the strain hardening elastic-plastic range. The finite element displacement method is used to perform the linear analyses in the iterative scheme. Bar and constant strain isotropic plane stress triangles are available for use in constructing structural idealizations. The use of ten different sets of material properties, three different material laws, and incremental proportional loading are available as options. Good correlation is shown with available test data and theoretical solutions.
|
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‡aMode of access: Internet.
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‡awill digitize
‡c20200915
‡zQueued for digitization
‡cSeptember 15, 2020
‡5miu
‡2pda
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‡aComputer programs.
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‡aElasticity.
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‡aStrains and stresses.
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‡aPlates (Engineering)
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‡aSandhu, R.,
‡eauthor.
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‡aBerke, L.,
‡eauthor.
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‡aAir Force Flight Dynamics Laboratory (U.S.),
‡eissuing agency.
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‡aIIT Research Institute,
‡esponsor.
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‡aTechnical Report Archive & Image Library (TRAIL)
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‡b2024-06-09T17:31:40Z
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