Thermal behavior of a titanium honeycomb-core sandwich panel
By: William L. Ko and Raymond H. Jackson.
Contributors: Jackson, Raymond H.; Dryden Flight Research Facility.
Series: NASA technical memorandum -- 101732.
Publisher: NASA Ames Resarch Center, Dryden Flight Research Facility; National Technical Information Service, distributor]
Published: 1991
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 13
Subjects: Aerodynamic heating; Airframes; Titanium; Finite element method; Honeycomb cores; Stress analysis; Temperature effects; Thermal stresses; Titanium
Notes: Distributed to depository libraries in microfiche.

"January 1991."

Includes bibliographical references (p. 6).

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.