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A comparison of graphite/epoxy tape laminates and 2-D braided composites mechanical properties [microform] / Pierre J. Minguet and Christian K. Gunther.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Test methods for textile composites [microform] / Pierre J. Minguet, Mark J. Fedro, and Christian K. Gunther.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Novel matrix resins for composites for aircraft primary structure [microform] / E.P. Woo ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
1991
0 resources
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
0 resources
Compression strength of composite primary structural components [microform] : semiannual status report : performance period: May 1, 1994 to October 31, 1994 / Eric R. Johnson, principal investigator.
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Blacksburg, Va. : Aerospace and Ocean Engineering Dept., Virginia Polytechnic and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1994
0 resources
Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates [microform] : an annual progress report / prepared by E. Gail Guynn, Walter L. Bradley.
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College Station, Tex. : Center for Mechanics of Composites, Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1989
0 resources
Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates [microform] / Suresh K. Sharma and Bhavani V. Sankar.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Microstructure and properties of cryomilled nickel aluminide extruded with chromium or molybdenum [microform] / Beverly J.M. Aikin, Robert M. Dickerson, and Patricia O. Dickerson.
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[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
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
0 resources
A thermostructural analysis of a diboride composite leading edge [microform] / Tom Kowalski ... [et al.].
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Planetary and primitive object strength measurements and sampling apparatus [microform] : NASA #NAGW 2439, final report; February 1, 1991 through January 31, 1997 / Thomas J. Ahrens, principal investigator.
Text
Pasadena, Calif. : California Institute of Technology, Seismological Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Experimental characterization and micromechanical modeling of woven carbon/copper composites [microform] / Brett A. Bednarcyk, Christopher C. Pauly, and Marek-Jerzy Pindera.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites [microform] / K.J. Bowles.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen [microform] / J. Daniel Whittenberger ... [et al.].
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Low cost manufacturing approach of high temperature PMC components [microform] / Kevin Kannmacher.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
1997
0 resources
Isothermal fatigue, damage accumulation, and life prediction of a woven PMC [microform] / Andrew L. Gyekenyesi.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure [microform] / R. Keith Bird and Eric K. Hoffman.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Thermal/mechanical response of a polymer matrix composite at cryogenic temperatures [microform] / Karen S. Whitley and Thomas S. Gates.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2003]
2003
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS55059Compression failure mechanisms of composite structures [microform] / H. Thomas Hahn, Mohsen Sohi, and Suresh Moon.
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[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
1986
0 resources
Mechanical strength and thermophysical properties of PM212 [microform] : a high temperature self-lubricating powder metallurgy composite / Phillip M. Edwards, ... [et al.].
Text
[Cleveland, Ohio : Lewis Research Center, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS64162Concepts for improving the damage tolerance of composite compression panels [microform] / Marvin D. Rhodes, Jerry G. Williams.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS95389Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates [microform] / Jerry G. Williams.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS95394A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.
Text
Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
2011
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo24323Notched strength allowables and inplane shear strength of AS4/VRM-34 textile laminates / Ray W. Grenoble, William M. Johnston.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2013.
2013-10
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo50482Evaluation 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/gpo50839Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen / J. Daniel Whittenberger [and others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1998.
1998-7
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo83113The effect of impact damage next to holes on the bearing strength of carbon fiber laminates / A.T. Nettles.
Text
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, December 2019.
2019-12
1 resource
Available online
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