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1
An evaluation of the plasticity-induced crack-closure /
by Newman, J. C.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998

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Government Document Book
2
Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024
by Riddell, William T.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998

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Government Document Book
3
An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses
by Phillips, Edward P.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997

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Government Document Book
4
Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet
by Phillips, Edward P.
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
5
Analyses of fatigue crack growth and closure near threshold conditions for large-crack behavior
by Newman, J. C.
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
6
Properties of aluminum alloys : fatigue data and the effects of temperature, product form, and processing /
by Kaufman, J. G. (John Gilbert), 1931-
Materials Park, Ohio : ASM International, 2008

Book
8
Strain hardening at large strains in aluminum alloys /

Thesis Book
9
Prediction of fatigue-crack-propagation behavior in panels with simulated rivet forces /

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Government Document Book
10
Factors influencing low-cycle crack growth in 2014-T6 aluminum sheet at -320° F (77 K) /
by Pierce, William S., Sullivan, Timothy L.
Washington, D.C. : National Aeronautics and Space Administration, 1969

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Government Document Book
11
Prediction of fatigue-crack growth in a high-strength aluminum alloy under variable-amplitude loading /
by Newman, J. C.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1989

Government Document Book
12
Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024 /
by Riddell, William T.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998

Government Document Book
13
Fatigue crack propagation in cylindrical shells,
by Catanach, W. M., Erdogan, F. (Fazil)
[Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 1968

Government Document Book
14
Guidelines for proof test analysis /
[Marshall Space Flight Center], Ala. : [Springfield, Va.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [National Technical Information Service, distributor], 1999

Government Document Book
15
Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy /
by Dawicke, David S.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997

Government Document Book
16
Periodic overload and transport spectrum fatigue crack growth tests of Ti62222STA and Al2024T3 sheet /
by Phillips, Edward P.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999

Government Document Book
17
An evaluation of the plasticity-induced crack-closure concept and measurement methods /
by Newman, J. C.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, 1998

Government Document Book
18
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
19
A study of fatigue and fracture in 7075-T6 aluminum alloy in vacuum and air environments /
by Hudson, Charles Michael, 1935-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book
20
Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys /
by Everett, Richard A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
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