Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications
By: D.R. Ambur.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 109175.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft structures.; Buckling.; Foams.; Impact resistance.; Panels.; Reinforcement (Structures); Stiffness.; Structural design.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0615-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.