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1
A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading
by Krueger, Ronald
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
2
A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading /
by Krueger, Ronald
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999

Government Document Book
3
Analysis of matrix cracking and local delamination in (O/[theta]-[theta][subscript] graphite epoxy laminates under tension load /
by Salpekar, Satish A. (Satish Annaji), 1954-
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R & T Activity ; [National Technical Information Service, distributor], 1991

Government Document Book
4
Analysis of local delaminations caused by angle ply matrix cracks /
by Salpekar, Satish A.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1993

Government Document Book
5
Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness /
by Li, Jian
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995

Government Document Book
6
Fatigue delamination onset prediction in tapered composite laminates /
by Murri, Gretchen B. (Gretchen Bostaph)
Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity, 1989

Government Document Book
7
Interlaminar fracture toughness of thermoplastic composites /
by Hinkley, Jeffrey A.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986

Government Document Book
8
Interlaminar shear fracture toughness and fatigue thresholds for composite materials /
by O'Brien, T. Kevin
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1987

Government Document Book
9
Local delamination in laminates with angle ply matrix cracks.
by O'Brien, T. Kevin
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R & T Activity, 1991

Government Document Book
10
Residual thermal and moisture influences on the strain energy release rate analysis of local delaminations from matrix cracks /
by O'Brien, T. Kevin
Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity, 1991

Government Document Book
11
Towards a damage tolerance philosophy for composite materials and structures /
by O'Brien, T. Kevin
Hampton, Va. : [St. Louis, MO] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity, 1988

Government Document Book
12
Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads /
by Hinkley, Jeffrey A.
Hampton, Va. : [St. Louis, Mo.] : [Springfield, Va.?] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity ; [National Technical Information Service [distributor], 1992

Government Document Book
13
Fatigue life methodology for tapered composite flexbeam laminates /
by Murri, Gretchen B. (Gretchen Bostaph)
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997

Government Document Book
14
Comparisons of various configurations of the edge delamination test for interlaminar fracture toughness /
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985

Government Document Book
15
Local delamination in laminates with angle ply matrix cracks.
by O'Brien, T. Kevin
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R & T Activity, 1991

Government Document Book
16
Results of ASTM round robin testing for mode I interlaminar fracture toughness of composite materials /
by O'Brien, T. Kevin
Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity, 1992

Government Document Book
17
Test and analysis of composite hat stringer pull-off test specimens /
by Li, Jian
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996

Government Document Book
18
Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load /
by Salpekar, Satish A. (Satish Annaji), 1954-
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R & T Activity ; [National Technical Information Service, distributor], 1990

Government Document Book
19
Influence of specimen preparation and specimen size on composite transverse tensile strength and scatter /
Hampton, Va. : Hanover MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001

Government Document Book
20
Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method /
by Salpekar, Satish A. (Satish Annaji), 1954-
Hampton, Va. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1987

Government Document Book
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