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Title Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners [electronic resource] / Wesley C.H. Slemp ... [et al.].

Imprint Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]

Copies

Location Call No. OPAC Message Status
 Axe Fed Docs - Online Documents  NAS 1.60:2011-217178    ---  Available
Description 1 online resource (39 p.) : ill. (some col.)
Series NASA/TP ; 2011-217178
NASA technical paper ; 2011-217178.
Note Title from title screen (viewed on Mar. 8, 2012).
"September 2011."
Bibliography Includes bibliographical references (p. 22-23).
Funding Sponsored by National Aeronautics and Space Administration 561581.02.08.07.15.15
L-20075
Subject Buckling.
Finite element method.
Design optimization.
Load tests.
Elastic buckling.
Wing panels.
Fixtures.
Deflection.
Loads (forces).
Added Author Slemp, Wesley C. H.
Langley Research Center.
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.60:2011-217178

 
    
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