Accuracies of Southwell and force/stiffness methods in the prediction of buckling strength of hypersonic aircraft wing tubular panels
By: William L. Ko.
Contributors: Dryden Flight Research Facility.
Series: NASA technical memorandum -- 88295.
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility; For sale by the National Technical Information Service]
Published: 1988
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings.; Buckling (Mechanics)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.