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  • Thermomechanical fatigue damage/failure mechanisms in SCS-6/timetal 21S [0/90]s composite [microform] / Michael G. Castelli.

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

  • Orientation effects on the measurement and analysis of critical CTOA in an aluminum alloy sheet [microform] / M.A. Sutton, D.S. Dawicke, J.C. Newman.

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

  • 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

  • Stress analysis of 27% scale model of AH-64 main rotor hub [microform] / Robert V. Hodges.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Retardation analytical model to extend service life [microform] : monthly technical progress narrative, month of August 1984 / prepared for National Aeronautics & Space Administration, Marshall Space Flight Center ; prepared by D. Matejczyk.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [1984]
    • 1984

  • Elevated temperature biaxial fatigue [microform] : semi-annual status report / principal investigator, Eric H. Jordan.

    • Text
    • Storrs, CT : Dept. of Mechanical Engineering, University of Connecticut ; [Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration, 1983]
    • 1983

  • Composite structural materials [microform] : semi-annual progress report, September 30, 1982 through April 30, 1983 / Air Force Office of Scientific Research and National Aeronautics and Space Administration ; co-principal investigators: George S. Ansell, Robert G. Loewy, and Stephen E. Wiberley.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1983]
    • 1983

  • Composite structural materials [microform] : semi-annual progress report, September 30, 1983 through April 30, 1984 / Air Force Office of Scientific Research and National Aeronautics and Space Administration ; co-principal investigators: George S. Ansell, Robert G. Loewy, and Stephen E. Wiberley.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
    • 1984

  • Three-dimensional measurements of fatigue crack closure [microform] : semi-annual status report / submitted by A.F. Grandt, Jr.

    • Text
    • [Washington, D.C.? : National Aeronautics and Space Administration, 1984]
    • 1984

  • Fatigue failure of regenerator screens in a high frequency Stirling engine [microform] / David R. Hull ... [et al.].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92492

  • Results of the round robin on opening-load measurement [microform] : conducted by ASTM Task Group E24.04.04 on crack closure measurement and analysis / Edward P. Phillips.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93125

  • Repeatability of mixed-mode adhesive debonding [microform] / R.A. Everett, Jr. and W.S. Johnson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : United States Army Aviation Systems Command, [1984]
    • 1984

  • Computer programs to characterize alloys and predict cyclic life using the total strain version of strainrange partitioning [microform] : tutorial and users manual : version 1.0 / James F. Saltsman.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97556

  • Complexities of high temperature metal fatigue--some steps toward understanding [microform] / S. S. Manson and G. R. Halford.

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

  • Use of the WEST-1 wind turbine simulator to predict blade fatigue load distribution [microform] / David C. Janetzke.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS100896

  • 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

  • Fatigue crack growth study of SCS₆/Ti-15-3 composite [microform] / Peter Kantzos and Jack Telesman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS108248

  • Time dependency of strainrange partitioning life relationships [microform] / Sreeramesh Kalluri and S.S. Manson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Three-dimensional elastic-plastic finite-element analysis of fatigue crack propagation [microform] / by R.G. Chermahini and G.L. Goglia.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, [1985]
    • 1985

  • Anisotropic constitutive model for nickel base single crystal alloys [microform] : development and finite element implementation / by L. Thomas Dame and D.C. Stouffer.

    • Text
    • Cincinnati, Ohio : University of Cincinnati ; [Washington, D.C.] : National Aeronautics and Space Administration, [1986]
    • 1986

  • Theoretical and software considerations for nonlinear dynamic analysis [microform] / by Richard J. Schmidt, Robert H. Dodds Jr.

    • Text
    • Lawrence, Kan. : University of Kansas Center for Research, [1983]
    • 1983

  • 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

  • Fatigue crack growth study of SCS₆/Ti-15-3 composite [microform] / Peter Kantzos and Jack Telesman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1989]
    • 1989

  • Time dependency of strainrange partitioning life relationships / Sreeramesh Kalluri and S.S. Manson.

    • Text
    • Cleveland, Ohio : Case Western Reserve University : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45893

  • Development and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions / Ronald Krueger.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : National Institute of Aerospace, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo23295

  • Grain boundary oxidation and oxidation accelerated fatigue crack nucleation and propagation / H. W. Liu and Yoshiki Oshida.

    • Text
    • Syracuse, N.Y. : Syracuse University, Dept. of Mechanical and Aerospace Engineering ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo23763

  • Fatigue crack growth under general-yielding cyclic-loading / Zheng Minzhong and H.W. Liu.

    • Text
    • Syracuse, N.Y. : Syracuse University, Dept. of Mechanical and Aerospace Engineering ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo23781

  • Fatigue crack growth under general-yielding cyclic-loading [microform] / Zheng Minzhong and H.W. Liu.

    • Text
    • Syracuse, N.Y. : Syracuse University, Dept. of Mechanical and Aerospace Engineering ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986

  • Grain boundary oxidation and oxidation accelerated fatigue crack nucleation and propagation [microform] / H.W. Liu and Yoshiki Oshida ; [performing organization: Syracuse University, Dept. of Mechanical and Aerospace Engineering ; sponsoring agency: National Aeronautics and Space Administration].

    • Text
    • Syracuse, N.Y. : Syracuse University, Dept. of Mechanical and Aerospace Engineering ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, [1986]
    • 1986

  • Investigation of methods for selectively reinforcing aluminum and aluminum-lithium materials / R. Keith Bird [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo47606

  • Mitigation of crack damage in metallic materials / Patrick Leser [and seven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2014.
    • 2014-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52361

  • Multilayer pressure vessel materials testing and analysis. Phase 1 / Joseph W. Cardinal, Carl F. Popelar and Richard A. Page.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53613

  • Multilayer pressure vessel materials testing and analysis. Phase 2 / Carl F. Popelar and Joseph W. Cardinal.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
    • 2014-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53612

  • Fatigue resistance of liquid-assisted self-repairing aluminum alloys reinforced with shape memory alloys : Shape Memory Alloy Self-Healing (SMASH) technology for aeronautical applications / M. Clara Wright, Dr. Michele Manuel, Dr. Terryl Wallace.

    • Text
    • [Cocoa Beach, FL] : [NASA Kennedy Space Center], September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54681

  • Test methodology development for experimental structural assessment of ASC planar spring material for long-term durability / Gunjin Yun [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2014.
    • 2014-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo56119

  • Time-temperature-stress capabilities of composite materials for advanced supersonic technology application / J.R. Kerr and J.F. Haskhs.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1987.
    • 1987-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo63151

  • Time-temperature-stress capabilities of composite materials for advanced supersonic technology application / J.R. Kerr and J.F. Haskhs.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1987.
    • 1987-5

  • Effect of notches on creep-fatigue behavior of a P/M nickel-based superalloy / Jack Telesman [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2015.
    • 2015-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64660

  • Investigation of spiral bevel gear condition indicator validation via AC-29-2C combining test rig damage progression data with fielded rotorcraft data / Paula J. Dempsey.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65847

  • An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses / Edward P. Phillips.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 1997.
    • 1997-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65690

  • Advanced face gear surface durability evaluations / David G. Lewicki, Gregory F. Heath.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; ARL, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68599

  • Estimation of slow crack growth parameters for constant stress-rate test data of advanced ceramics and glass by the individual data and arithmetic mean methods / Sung R. Choi, Jonathan A. Salem and Frederic A. Holland.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69782

  • Contact and bending durability calculation for spiral-bevel gears / Sandeep Vijayakar.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2016.
    • 2016-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72487

  • Materials characterization of electron beam melted Ti-6Al-4V / Susan L. Draper [and six others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2016.
    • 2016-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73032

  • Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / C.E. Harris [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67204

  • Application of machine learning to rotorcraft health monitoring / Tyler Cody, Paula J. Dempsey.

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2017.
    • 2017-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78192

  • Reaction and protection of electrical wire insulators in atomic-oxygen environments / Ching-cheh Hung and Gidget Cantrell.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1994.
    • 1994-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79545

  • An evaluation of the plasticity-induced crack-closure concept and measurement methods / James C. Newman, Jr.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1998.
    • 1998-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83238

  • A practical engineering approach to predicting fatigue crack growth in riveted lap joints / C.E. Harris, R.S. Piascik and J.C. Newman, Jr.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2000.
    • 2000-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86065

  • Fatigue crack growth characteristics of thin sheet titanium alloy Ti 6-2-2-2-2 / Stephen W. Smith and Robert S. Piascik.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2001.
    • 2001-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22882

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