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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
Description
Item Description:Distributed to depository libraries in microfiche.
"January 1991."
Microform.
Physical Description:13 pages : charts ; 28 cm.
Also available via Internet from the NTRS web site. Address as of 5/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910008120%5F1991008120.pdf; current access is available via PURL.
Bibliography:Includes bibliographical references (page 6).