Thermal behavior of a titanium honeycomb-core sandwich panel /

Bibliographic Details
Main Author:	Ko, William L.
Corporate Author:	Dryden Flight Research Facility
Other Authors:	Jackson, Raymond H.
Format:	Government Document Book
Language:	English
Published:	Edwards, Calif. : NASA Ames Resarch Center, Dryden Flight Research Facility ; 1991.
Series:	NASA technical memorandum ; 101732.
Subjects:	Aerodynamic heating. Airframes. Titanium. Finite element method. Honeycomb cores. Stress analysis. Temperature effects. Thermal stresses.
Online Access:	https://purl.fdlp.gov/GPO/LPS60262