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Flow separation in shock wave boundary layer interactions at hypersonic speeds

Hamed, A. (Awatef)
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, 1990]. 1990

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 de

Prabhu, Ramadas K.
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001] 2001

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF

Perkins, H. Douglas, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

On the instability of hypersonic flow past a flat plate

Blackaby, Nicholas D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Optimal trajectories for an aerospace plane

Miele, Angelo.
Houston, Tex. : Rice University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

Quantitative global heat transfer in a Mach-6 quiet tunnel

Sullivan, John P., author.
Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

X-15 : extending the frontiers of flight

Jenkins, Dennis R., author.
Washington D.C. : National Aeronautics and Space Administration, NASA Headquarters, [2007] 2007