Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /

Bibliographic Details

Main Author:	Ko, William L. (Author)
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
Series:	NASA technical memorandum ; 4770.
Subjects:	Aircraft structures. Thermal buckling. Mechanical properties. Finite element method. Hypersonic aircraft.
Online Access:	https://purl.fdlp.gov/GPO/gpo65666