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E-Book/E-Doc

Title Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners [electronic resource] / Sameer B. Mulani ... [et al.].

Imprint

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]

Connect to
Connect to https://permanent.fdlp.gov/gpo31180/20120011954_2012011764.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120011954.pdf

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:2012-217584	---	Available

Description	1 online resource (x, 33 p.) : ill. (some col.)
Series	NASA/TP ; 2012-217584
	NASA technical paper ; 2012-217584.
Note	Title from title screen (viewed on Nov. 13, 2012).
	"June 2012."
Bibliography	Includes bibliographical references (p. 20-22).
Funding	Sponsored by National Aeronautics and Space Administration 561581.02.08.07.43.01
	L-20156
Subject	Design optimization.
	Finite element method.
	Photogrammetry.
	Aluminum alloys.
	Digital systems.
	Displacement.
	Buckling.
Added Author	Mulani, Sameer B.
	Langley Research Center.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:2012-217584