NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of temperature change on optimum laminate designResults of a laminate optimization study, which includes prescribed temperature change and mechanical loading conditions, are presented. Minimum-weight designs for balanced symmetric laminates are obtained subject to strength, membrane stiffness, and minimum thickness requirements, while including and omitting temperature change effects. Based on a first ply failure design philosophy and employing a linear thermoelastic analysis, it is shown that taking temperature decrease effects into account leads to substantial weight penalties in strength critical fiber composite laminates. Numerical results are presented for representative fiber composite materials based on three commonly used combined stress failure criteria.
Document ID
19770064235
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schmit, L. A., Jr.
(California, University Los Angeles, Calif., United States)
Tashkandi, M. A.
(California Univ. Los Angeles, CA, United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1977
Publication Information
Publication: AIAA Journal
Volume: 15
Subject Category
Structural Mechanics
Accession Number
77A47087
Funding Number(s)
CONTRACT_GRANT: NGR-05-007-337
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available