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  • Analysis of some compliance calibration data for chevron-notch bar and rod specimens [microform] / Thomas W. Orange ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • Computer modeling the fatigue crack growth rate behavior of metals in corrosive environments [microform] / Edward Richey, III ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The role of crack formation in chevron-notched four-point bend specimens [microform] / Anthony M. Calomino, and Louis J. Ghosn.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Implementation of and measurement with the LIPA technique in a subsonic jet [microform] : final report / R.E. Falco.

    • Text
    • East Lansing, MI : Michigan State University, Dept. of Mechanical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The crack problem in bonded nonhomogeneous materials [microform] / by F. Erdogan, A.C. Kaya, P.F. Joseph.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance [microform] / edited by Charles E. Harris.

    • Text
    • [Hampton, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994- ]
    • 1994-present

  • Driving force analysis in an infinite anisotropic plate with multiple crack interactions [microform] / Wieslaw K. Binienda and Steven M. Arnold.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Multi-lab comparison of R-curve methodologies [microform] : alloy 2024-T3 / Anthony P. Reynolds.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The crack problem in a reinforced cylindrical shell [microform] / O. Selcuk Yahsi and F. Erdogan.

    • Text
    • Bethlehem, Penn. : Lehigh University ; [Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Stress analysis of Pathfinder-II models [microform] / S.C. Mehrotra and C.T.L. Mills.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Stress intensity factor in a tapered specimen [microform] / Liu Xue-Hui and F. Erdogan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • Fracture analysis of notched composites [microform] / F. Delale.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Analysis of corner cracks at hole by a 3-D weight function method with stresses from finite element method [microform] / W. Zhao ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Analysis of surface cracks at hole by a 3-D weight function method with stresses from finite element method [microform] / W. Zhao ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Fatigue-life prediction methodology using small-crack theory [microform] / J.C. Newman, Jr. and E.P. Phillips, M.H. Swain.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • FASTRAN-II [microform] : a fatigue crack growth structural analysis program / J.C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992

  • The merging of fatigue and fracture mechanics concepts [microform] : a historical perspective / J.C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Determination of stress intensity factor distributions for "interface" cracks in incompressible, dissimilar materials [microform] : summary report : reporting period - 8/15/94 - 12/31/97 : grant no. NAG-1-1622-Supl. 1-5* / C.W. Smith, P.I.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Determination of stress coefficient terms in cracked solids for monoclinic materials with plane symmetry at x₃=0 [microform] / F.G. Yuan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • A back face strain compliance expression for the compact tension specimen [microform] / William T. Riddell and Robert S. Piascik.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Fatigue analyses under constant- and variable-amplitude loading using small-crack theory [microform] / J.C. Newman, Jr. and E.P. Phillips; R.A. Everett, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Analysis of multiple cracks in an infinite functionally graded plate [microform] / N.I. Shbeeb, W.K. Vinienda, and K.L. Kreider.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Analysis of an interface crack for a functionally graded strip sandwiched between two homogeneous layers of finite [microform] / N.I. Shbeeb and W.K. Binienda

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads [microform] / James H. Starnes, Jr. ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Analysis of a generally oriented crack in a functionally graded strip sandwiched between two homogeneous half planes [microform] / N. Shbeeb, W.K. Binienda, and K. Kreider.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Stress-intensity factor equations for cracks in three-dimensional finite bodies subjected to tension and bending loads [microform] / J. C. Newman, Jr. and I. S. Raju.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54979

  • Frequency domain analysis of the random loading of cracked panels [microform] / James F. Doyle.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60774

  • Fatigue crack growth in unidirectional metal matrix composite [microform] / Louis J. Ghosn, Jack Telesman and Peter Kantzos ; prepared for the International Fatigue Series (FATIGUE 90), Honolulu, Hawaii, July 15-20, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61905

  • Through-the-thickness fatigue crack closure behavior in an aluminum alloy [microform] / D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62877

  • Fatigue crack initiation and small crack growth in several airframe alloys [microform] / M.H. Swain ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69445

  • Influence of fatigue crack wake length and state of stress and on crack closure [microform] / Jack Telesman and Douglas M. Fisher.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986

  • Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet [microform] / C.A. Bigelow.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • A cylindrical shell with a stress-free end which contains an axial part-through or through crack [microform] / F. Erdogan and O.S. Yahsi.

    • Text
    • Bethlehem, Pa. : Lehigh University ; [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • A pressurized cylindrical shell with a fixed end which contains an axial part-through or through crack [microform] / by O .S. Yahsi and F. Erdogan.

    • Text
    • Bethlehem, PA : Lehigh University ; [Washington, DC] : National Aeronautics and Space Administration, [1983]
    • 1983

  • Surface cracks in a plate of finite width under tension or bending [microform] / F. Erdogan and H. Boduroglu.

    • Text
    • Bethlehem, Pa. : Lehigh University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • The crack-inclusion interaction problem [microform] / Liu Xue-Hui and F. Erdogan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Stress intensity factors in a reinforced thick-walled cylinder [microform] / Renji Tang and F. Erdogan.

    • Text
    • Bethlehem, Pa. : Lehigh University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • The Dugdale model for the compact specimen [microform] / S. Mall, J. C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983

  • Resin selection criteria for "tough" composite structures [microform] / C.C. Chamis and G.T. Smith.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • Resin selection criteria for tough composite structures [microform] / C.C. Chamis and G.T. Smith.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • Experimental compliance calibration of the NASA Lewis Research Center Mode II fatigue specimen [microform] / Robert J. Buzzard.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985

  • Plates and shells containing a surface crack under general loading conditions [microform] / Paul F. Joseph and Fazil Erdogan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987

  • Interaction of part-through cracks in a flat plate / B. Aksel and F. Erdogan.

    • Text
    • Bethlehem, Pennsylvania : Lehigh University ; Hampton. Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1985.
    • 1985-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo48086

  • Characterization of residual stress effects on fatigue crack growth of a friction stir welded aluminum alloy / John A. New [and seven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57876

  • Effects of aqueous solutions on slow crack growth of soda-lime-silicate glass / Bronson D. Hausmann, Jonathan A. Salem.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2016.
    • 2016-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66957

  • Resin selection criteria for "tough" composite structures / C.C. Chamis and G.T. Smith.

    • Text
    • [Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1983]
    • 1983
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo74377

  • A back face strain compliance expression for the compact tension specimen / William T. Riddell and Robert S. Piascik.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 1998.
    • 1998-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83265

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