Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels
By: Navin Jaunky and Norman F. Knight, Jr., Damodar R. Ambur.
Contributors: Knight, Norman F.; Ambur, Damodar R.; Langley Research Center.
Series: NASA technical memorandum -- 110162.
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: Aerospace engineering.; Buckling.; Composite structures.; Computer programs.; Finite element method.; Rayleigh-Ritz method.; Reinforced plates.; Static loads.; Stiffening.; Stiffness.; Structural engineering.; Webs (Support)
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0033-M.

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