Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners
By: Wesley C.H. Slemp ... [et al.].
Contributors: Langley Research Center
Series: NASA/TP -- 2011-217178; NASA technical paper -- 2011-217178.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 2011
Place of publication: Hampton, Va
Language: eng
Format: [electronic resource] /
Number of pages: 39
Subjects: Loads (forces); Buckling; Finite element method; Design optimization; Load tests; Elastic buckling; Wing panels; Fixtures; Deflection
Notes: Title from title screen (viewed on Mar. 8, 2012).

"September 2011."

Includes bibliographical references (p. 22-23).

Sponsored by National Aeronautics and Space Administration 561581.02.08.07.15.15

L-20075