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Displaying 1-13 of 13 results
Concept development of a Mach 2.4 high-speed civil transport [microform] / James W. Fenbert ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Study of high-speed civil transports [microform] / Douglas Aircraft Company, New Commercial Programs.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS63775Inlet flowfield investigation. Part I. Transonic flowfield survey [microform].
- Text
- Seattle, Wash. : Boeing Military Airplane Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
- 1983
High altitude turbulence for supersonic cruise vehicles [microform] / L. J. Ehernberger.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.
- 1987
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS92585Development and analysis of a STOL supersonic cruise fighter concept [microform] / Samuel M. Dollyhigh, ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
- 1984
Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration [microform] / David E. Hahne.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS97104Supersonic cruise technology [microform] / F. Edward McLean.
- Text
- Washington, D.C. : NASA Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985.
- 1985
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS101643Theoretical and experimental flow fields for a supersonic cruise fighter forebody [microform] / Steven F. Yaros.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
- 1985
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [electronic resource] / A.G. Powell, S. Agrawal, T. R. Lacey.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS113610Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS113610Preliminary design of a supersonic cruise aircraft high-pressure turbine [microform] : final report / [prepared by L.D. Aceto, J.C. Calderbank].
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1983]
- 1983
Preliminary design of a supersonic cruise aircraft high-pressure turbine : final report / L. D. Aceto, J. C. Ca1derbank.
- Text
- [Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1983]
- 1983
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo21282Global environmental impact of supersonic cruise aircraft in the stratosphere / Raymond L. Speth [and seven others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2021.
- 2021-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo151988
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