Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Slemp, Wesley C. H.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:	NASA technical paper ; 2011-217178.
Subjects:	Buckling. Finite element method. Design optimization. Load tests. Elastic buckling. Wing panels. Fixtures. Deflection. Loads (Forces)
Online Access:	https://purl.fdlp.gov/GPO/gpo19822