The buckling response of symmetrically laminated composite plates having a trapezoidal planform area
By: H.D. Radloff II, M.W. Hyer, M.P. Nemeth.
Contributors: Hyer, M. W.; Nemeth, Michael P.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-196975.; Interim report -- 98.; Interim report (NASA-Virginia Tech. Composites Program) -- 98.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Buckling.; Finite element method.; Graphite-epoxy composites.; Laminates.; Plates (Structural members); Rayleigh-Ritz method.; Trapezoids.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0268-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.