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Displaying 1-4 of 4 results
Computational simulation of damage progression of composite thin shells subjected to mechanical loads [microform] / P.K. Gotsis, C.C. Chamis, L. Minnetyan.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell [microform] / Naveen Rastogi and Eric R. Johnson.
- Text
- Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS60750PRSEUS pressure cube test data and response / Andrew E. Lovejoy.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo37999
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