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

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

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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 Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989. [Washington, DC] : [Springfield, VA] : 1989.
Series:	NASA technical memorandum 4139.
Subjects:	Composite materials > Delamination. Bars. Bending. Composite materials. Delaminating. Loads (forces) Performance prediction. Stress analysis.

University of Minnesota

Holdings details from University of Minnesota
Call Number:	Mfiche NAS 1.15:4139

Winona State University

Holdings details from Winona State University
Call Number:	TL521.3.T4