Research Catalog

  • Elastic modulus measurements of LDEF glasses and glass-ceramics using a speckle technique [microform] / D.E. Wiedlocher and D.L. Kinser.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Finite element analysis of a composite wheelchair wheel design [microform] / Rene Ortega.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Reliability-based failure analysis of brittle materials [microform] / Lynn M. Powers and Louis J. Ghosn.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • Shear buckling analysis of a hat-stiffened panel [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994
  • Improvements to a method for the geometrically nonlinear analysis of compressively loaded stiffened composite panels [microform] : progress report for the period July 1991 to December 1991.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Center, distributor, 1991]
    • 1991
  • Nonlinear analysis for the response and failure of compression-loaded angle-ply laminates with a hole [microform] / Steven R. Mathison ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Micromechanics of composite laminate compression failures [microform] : semi-annual progress report for NASA research grant NAG-1-659, (for work through November 1, 1986) / prepared by E. Gail Guynn, Walter L. Bradley.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Test load verification through strain data analysis [microform] / V. Verderaime and F. Harrington.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Micromechanics of compression failures in open hole composite laminates [microform] : a report / by E. Gail Guynn, Walter L. Bradley.

    • Text
    • College Station, Tex. : Mechanics and Materials Center, Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Fatigue response of notched laminates subjected to tension-compression cyclic loads [microform] / C.E. Bakis, W.W. Stinchcomb.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Prestraining and its influence on subsequent fatigue life [microform] / Sreeramesh Kalluri, Gary R. Halford, and Michael A. McGaw.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box [microform] / D.C. Jegley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Analytical comparison of three stiffened panel concepts [microform] / Jill M. Maloney and K. Chauncey Wu, James C. Robinson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Discontinuously stiffened composite panel under compressive loading [microform] / Levon Minnetyan ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy [microform] / Alan T. Nettles.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep [microform] / Thomas S. Gates, David R. Veazie, L. Catherine Brinson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy [microform] / David S. Dawicke.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Torsional buckling tests of a simulated solar array [microform] : a final report, grant no. NAG5-2924, June 1, 1995-August 31, 1996 / submitted by E.A. Thornton.

    • Text
    • Charlottesville, VA : School of Engineering & Applied Science, University of Virginia ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading [microform] / : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / David M. McGowan and Damodar R. Ambur.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Investigation of anomalous behavior in metallic-based materials under compressive loading [microform] / Christopher M. Gil and Cliff J. Lissenden, Bradley A. Lerch.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Identification of nonlinear micron-level mechanics for a precision deployable joint [microform] / S.J. Bullock and L.D. Peterson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • TSS-1R mission failure investigation board [microform] : final report.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1996
  • Progressive failure studies of composite panels with and without cutouts [microform] / Navin Jaunky ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39065
  • Fabrication and evaluation of superplastically formed/weld-brazed corrugated compression panels with beaded webs [microform] / Dick M. Royster ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985
  • Measure of displacement around holes in composite plates subjected to quasi-static compression [microform] / John C. Duke, Jr., ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986
  • Short-wavelength buckling and shear failures for compression-loaded composite laminates [microform] / Mark J. Shuart.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85692
  • Analytical results for postbuckling behavior of plates in compression and in shear [microform] / Manuel Stein.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
  • Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [electronic resource] / Anthony Waas and Charles Babcock, Jr.

    • Text
    • Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112451
  • Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [microform] / Anthony Waas and Charles Babcock, Jr.

    • Text
    • Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112451
  • Delamination growth in composite materials [microform] / John W. Gillespie, Jr. ... [et al.].

    • Text
    • Newark, Del. : Center for Composite Materials ; [Washington, D.C. : National Aeronautics and Space Administration, 1985?]
    • 1985
  • Delamination growth in composite materials / John W. Gillespie, Jr ... [and others].

    • Text
    • Newark, Del. : Center for Composite Materials, College of Engineering, University of Delaware ; [Washington, D.C.] : National Aeronautics and Space Administration, [1985?]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo21423
  • Effect of stress concentrations in composite structures : progress report / by C.D. Babcock and A.M. Waas.

    • Text
    • Pasadena CA : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, DC] : [National Aeronautics and Space Administration], [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo22122
  • Effect of stress concentrations in composite structures [microform] : progress report / by C.D. Babcock and A.M. Waas.

    • Text
    • Pasadena CA : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration, 1985]
    • 1985
  • Delamination growth in composite materials / John W. Gillespie, Jr ... [and others].

    • Text
    • Newark, Del. : University of Delaware, Center for Composite Materials, College of Engineering ; Hampton,Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24058
  • Delamination growth in composite materials [microform] / John W. Gillespie, Jr. ... [et al.].

    • Text
    • Newark, Del. : University of Delaware, Center for Composite Materials, College of Engineering ; Hampton,Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
  • Rolling bearing steels : a technical and historical perspective / Erwin V. Zaretsky.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27889
  • Evaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens / Dawn C. Jegley.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo50839
  • Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.

    • Text
    • Pasadena, California : California Institute of Technology, August, 1987.
    • 1987-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57134
  • Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.

    • Text
    • Pasadena, California : California Institute of Technology, August, 1987.
    • 1987-8
  • An overview of advanced elastomeric seal development and testing capabilities at NASA Glenn Research Center / Patrick H. Dunlap, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
    • 2014-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57562
  • Advanced gear alloys for ultra high strength applications / Tony Shen, Timothy Krantz, Jason Sebastian.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2011.
    • 2011-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33398
  • Acoustic emission monitoring of the DC-XA composite liquid hydrogen tank during structural testing / C. Wilkerson.

    • Text
    • MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67653
  • Design and use of a guided weight impactor to impart barely visible impact damage / Andrew E. Lovejoy, Adam Przekop.

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, April 2016.
    • 2016-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69169
  • Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009 / Mark W. Hilburger [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82549
  • Design and manufacture of elastically tailored tow placed plates / Brian F. Tatting, Zafer Gürdal.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [2002]
    • 2002
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60511
  • A comparison of candidate seal designs for future docking systems / Patrick H. Dunlap, Jr. and Bruce M. Steinetz.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37230
  • Normalization of impact energy by laminate thickness for compression after impact testing / A.T. Nettles and S.M. Hromisin.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37983

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta