Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces
By: William L. Ko
Contributors: Hugh L. Dryden Flight Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/TP -- 1999-206580; NASA technical paper -- 1999-206580.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; Available from NASA Center for AeroSpace Information
Published: 1999
Place of publication: Edwards, Calif; Hanover, Md
Language: eng
Number of pages: 37
Subjects: Aerothermodynamics; Composite materials -- Delamination; Composite materials -- Deterioration; Hypersonic planes -- Research; Sandwich construction -- Testing
Notes: "June 1999."

"Performing organization report number H-2332"--Report documentation page.

Includes bibliographical references.

Prepared by NASA Dryden Flight Research Center for National Aeronautics and Space Administration WU 242-33-02-00-23-00-TA1