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A computational fluid dynamics simulation of the hypersonic flight of the Pegasus (TM) vehicle using an artificial viscosity model and a nonlinear filtering method [microform] / John Cadiz Mendoza.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
1995
0 resources
Pegasus wing-glove experiment to document hypersonic crossflow transition [microform] : measurement system and selected flight results / Arild Bertelrud ... [et al.].
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
2000
0 resources
Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
1995
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo77772Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
1995
0 resources
Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / Arild Bertelrud [and ten others].
Text
Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, January 2000.
2000-1
1 resource
Available online
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