Research Catalog
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Displaying 1-18 of 18 results
Strain rate dependent modeling of polymer matrix composites [microform] / Robert K. Goldberg, Donald C. Stouffer.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Influence of ply waviness on fatigue life of tapered composite flexbeam laminates [microform] / Gretchen B. Murri.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
Use of photostress to analyze behavior of an aft skirt test specimen [microform] / prepared by S.C. Gambrell, Jr.
- Text
- Tuscaloosa, Ala. : The University of Alabama, College of Engineering, Bureau of Engineering Research ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Center, distributor, 1994]
- 1994
Treatment of singularities in cracked bodies [microform] / K.N. Shivakumar and I.S. Raju.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va., : National Technical Information Service, distributor, 1989]
- 1989
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
An evaluation of a coupled microstructural approach for the analysis of functionally graded composites via the finite-element method [microform] / Marek-Jerzy Pindera and Patrick Dunn.
- 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
U-groove aluminum weld strength improvement [microform] / V. Verderaime and R. Vaughan.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box [microform] / John T. Wang ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Property evaluation of LTM25 composite materials [microform] / A.S. Postyn and C.H. Shah.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Determination of yield in Inconel 718 for axial-torsional loading at temperatures up to 649⁰C [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
Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.
- Text
- Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, DC] : [National Aeronautics and Space Administration], [1984]
- 1984
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51595Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.
- Text
- Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, District of Columbia] : [National Aeronautics and Space Administration], [1984]
- 1984
Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains / William L. Ko and Van Tran Fleischer.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2013.
- 2013-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo49705U-groove aluminum weld strength improvement / V. Verderaime and R. Vaughan.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
- 1996
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo78956Curved displacement transfer functions for geometric nonlinear large deformation structure shape predictions / William L. Ko, and Van Tran Fleischer, Shun-Fat Lung.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, March 2017.
- 2017-3
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo79532Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test / Christine V. Jutte [and five others].
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
- 2011
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo34104Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains / William L. Ko and Van Tran Fleischer.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37308
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