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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.].

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

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Connect to https://permanent.fdlp.gov/gpo19822/20110016508-2011017519.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110016508.pdf

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	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