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1
The X-15 rocket plane : flying the first wings into space
Lincoln : University of Nebraska Press, 2013Format: Book
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2
Measured pressure distributions, aerodynamic coefficients, and shock shapes on blunt bodies at incidence in hypersonic air and CF₄
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1982Format: Government Document Book
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3
Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at Mach 1.60 to 2.87
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977Format: Government Document Book
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4
X-15 : extending the frontiers of flight
Washington DC : NASA, 2007Format: Book
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5
The Center of Excellence for Hypersonics Training & Research at the University of Texas at Austin : final report
[Washington, DC] : [National Aeronautics and Space Administration], 1993Format: Government Document Book
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6
Hypersonic flow
New York : Wiley, 1994Format: Book
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7
Hypersonic flows as related to the national aerospace plane : semi-annual research report for cooperative agreement no.: NCC2-452 for the period August 1, 1990 - February 28, 1991
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1991Format: Government Document Book
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8
Advanced computational techniques for hypersonic propulsion
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1989Format: Government Document Book
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9
Turbulence modeling for hypersonic flight
San Jose, Calif. : [Washington, DC] : [Springfield, Va.?] : MCAT Institute ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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10
Space shuttle hypersonic aerodynamic and aerothermodynamic flight research and the comparison to ground test results
[Washington, DC] : [Linthicum Heights, Md.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Available from the NASA Center for Aerospace Information], 1993Format: Government Document Book
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11
Hypersonic and high-temperature gas dynamics
Reston, Va. : American Institute of Aeronautics and Astronautics, 2006
2nd ed.Format: Book
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12
Instrumentation for hypersonic aerodynamics research with tethered satellites : final report fo the period January 1, 1990 to January 15, 1992
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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13
Aerodynamics of bodies of revolution
New York, American Elsevier Pub. Co., 1970Format: Book
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14
Studies of shock/shock interaction on smooth and transpiration-cooled hemispherical nosetips in hypersonic flow
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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15
Computation of H2/air reacting flowfields in drag-reduction external combustion
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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16
Hypersonic aerodynamic coefficients and convection flow estimation in a Hermes type project
Washington, DC : National Aeronautics and Space Administration, 1987Format: Government Document Book
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17
Enhancing U.S. competitiveness NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Sci...
Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1994Format: Government Document Book
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18
Normal- and oblique-shock flow parameters in equilibrium air : including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral
Washington : Springfield, Va. : Scientific and Technical Information Office, National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1975Format: Book
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19
Experimental methods of hypersonics
New York : M. Dekker, 1973Format: Book
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20
An explicit upwind algorithm for solving the parabolized Navier-Stokes equations
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1991Format: Government Document Book
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