Research Catalog
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Displaying 1-5 of 5 results
Critical joints in large composite aircraft structure [microform] / Willard D. Nelson, Bruce L. Bunin, and Leonard John Hart-Smith.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1983.
- 1983
Axisymmetric inlet minimum weight design method [microform] / Shari-Beth Nadell.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Continuum fatigue damage modeling for critical design, control, and fault prognosis [microform] / Carl F. Lorenzo.
- Text
- [Washington, DC] : 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
Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 : test dates: 19-21 November 2008 / Mark W. Hilburger, W. Allen Waters, Jr., Waddy T. Haynie.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
- 2015-8
- 1 Resource
Available Online
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