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Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments /

Bibliographic Details
Main Author: Ko, William L.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors: Jackson, Raymond H.
Format: Government Document Microform Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:NASA technical memorandum ; 4139.
Subjects:
Composite materials > Delamination.
Bars.
Bending.
Composite materials.
Delaminating.
Loads (Forces)
Performance prediction.
Stress analysis.
Online Access:https://purl.fdlp.gov/GPO/LPS70454

Internet

https://purl.fdlp.gov/GPO/LPS70454

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Call Number: NAS 1.15:4139
 
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