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1
Stresses around rectangular cut-outs with reinforced coaming stringers /
by Kuhn, Paul, Rafel, Norman, Griffith, George E.
Washington : National Advisory Committee for Aeronautics, 1947

Government Document Book
2
Determination of yield in Inconel 718 for axial-torsional loading at temperatures up to 649°C
by Gil, Christopher M.
[Cleveland, Ohio] : Springfield, VA : National Aeronautics and Space Administration, Lewis Research Center ; National Technical Information Service, distributor, 1998

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Government Document Book
3
Testing and analysis of composite skin/stringer debonding under multi-axial loading
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999

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Government Document Book
4
Flight-time identification of a UH-60A helicopter and slung load /
by Cicolani, Luigi S.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1998

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Government Document Book
5
Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects
by Paraska, Peter J.
Bethesda, MD : [Washington, DC : Springfield, Va. : Carderock Division, Naval Surface Warfare Center ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1993

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Government Document Book
6
Stress-strain response of fabrics under two-dimensional loading /
by Freeston, W. Denney
Natick, Mass. : General Equipment and Packaging Laboratory, U. S. Army Natick Laboratories, 1971

Book
7
Preliminary nonlinear structural analysis of advanced composite tow-steered shells with large geometric imperfections /
by Dobrin, Calvin P., Wu, K. Chauncey, Stanford, Bret K.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2019

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Government Document Book
8
A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads /
by Burke, Walter E.
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1935

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Government Document Book
9
Axial and torsional fatigue behavior of Waspaloy
by Zamrik, S. Y., 1932-
University Park, Pa. : [Cleveland, Ohio] : Pennsylvania State University, Engineering Science and Mechanics Department ; National Aeronautics and Space Administration, Lewis Research Center, 1986

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Government Document Electronic Book
10
Seismic loads /
by Li︠a︡tkher, V. M. (Viktor Mikhaĭlovich)
Hoboken, New Jersey ; Salem, Massachusetts : Scrivener Publishing : Wiley, 2016

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Book
11
Principal effects of axial load on moment-distribution analysis of rigid structures /
by James, Benjamin Wylie
Washington, [D.C.] : National Advisory Committee for Aeronautics, 1935

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Government Document Book
12
Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells : presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category /
by Johnson, Theodore F.
[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995

Government Document Book
13
Simplified method for calculating thermal conductance of rough, nominally flat surfaces in high vacuum /
by McKinzie, Daniel J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information], 1970

Government Document Book
14
Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects /
by Paraska, Peter J.
Bethesda, MD : [Washington, DC] : [Springfield, Va.] : Carderock Division, Naval Surface Warfare Center ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993

Government Document Book
15
Determination of energy release rate for biaxial brittle fracture specimen /
by Bush, A. J., Wilson, W. K.
Pittsburgh, Pennsylvania : Westinghouse Electric Corp., Research Labs, 1964

Book
16
Investigation of the applicability of the biaxial brittle fracture test for determining fracture toughness /
by Wessel, E. T., Pryle, W. H.
Pittsburgh, Pa. : Westinghouse Research Labs, 1965

Book
17
Fracture analysis of stiffened panels under biaxial loading with widespread cracking /
by Newman, J. C.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995

Government Document Book
18
J-integral estimates for cracks in infinite bodies /
by Dowling, Norman E.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1986

Government Document Book
19
Buckling and vibration analysis of a simply supported column with a piecewise constant cross section /
by Lake, Mark S.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1991

Government Document Book
20
Analysis and design of the NASA Langley cryogenic pressure box /
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999

Government Document Book
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