Buckling and damage resistance of transversely-loaded composite shells
By: by Brian L. Wardle.
Contributors: United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA/CR-208340.; NASA contractor report -- NASA CR-208340.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Composite structures.; Shells (Structural forms); Graphite-Epoxy composites.; Impact damage.; Shell stability.; Finite element method.; Mathematical models.; Structural analysis.; Transverse loads.; Laminates.; Impact resistance.
Notes: Shipping list no.: 99-0323.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 3 microfiches.