Research Catalog
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Displaying 1-12 of 12 results
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
SCARE--a post-processor program to MSC/NASTRAN for the reliability analysis of structural ceramic components [microform] / John P. Gyekenyesi.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Energy absorption by polymer crazing [microform] / S.S. Pang, ... [et al.].
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1983?]
- 1983
Transient thermal stresses in a reinforced hollow disk or cylinder containing a radial crack [microform] / by Renji Tang and F. Erdogan.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1983]
- 1983
Unit-sphere anisotropic multiaxial stochastic-strength model probability density distribution for the orientation of critical flaws / Noel N. Nemeth.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
- 2013-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo50521Multilayer 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/gpo53612Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code / David C. Lo [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/gpo65365Effects of fiber content on mechanical properties of CVD SiC fiber-reinforced strontium aluminosilicate glass-ceramic composites / Narottam P. Bansal.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
- 1996-7
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo69483Method for estimating crack-extension resistance curve from residual-strength data / Thomas W. Orange.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
- 1980-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo71176A 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/gpo83265Microprobe evaluations of grain boundary segregation in KM4 and IN100 / T.P. Gabb, J.W. Smith.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2001.
- 2001-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS26800Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer / Shantaram S. Pai, David S. Riha.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo40538
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