Search Results

1

Extraction of stability and control derivatives from orbiter flight data /

by Iliff, Kenneth W.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Book

2

Stagnation-point heat-transfer rate predictions at aeroassist flight conditions /

by Gupta, Roop N.
[Washington, DC] : [Springfield, Va.?] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1992

Government Document Book

3

A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients /

by Whitmore, Stephen A.
Washington, DC : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996

Book

4

Experimental investigation of generic three-dimensional sidewall-compression scramjet inlets at Mach 6 in tetrafluoromethane /

by Holland, Scott D. (Scott Douglas), 1964-
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993

Government Document Book

5

Space shuttle hypersonic aerodynamic and aerothermodynamic flight research and the comparison to ground test results /

by Iliff, Kenneth W.
[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], 1993

Government Document Book

6

Stagnation-point heat-transfer rate predictions at aeroassist flight conditions /

by Gupta, Roop N.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Book

7

Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation /

by Monta, William J.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992

Government Document Book

8

Space shuttle hypersonic aerodynamic and aerothermodynamic flight research and the comparison to ground test results /

by Iliff, Kenneth W.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Book

9

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 /

by Walker, Ira J.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993

Government Document Book

10

Computational parametric study of sidewall-compression scramjet inlet performance at mach 10 /

by Holland, Scott D. (Scott Douglas), 1964-
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Government Document Book

11

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation /

by Huebner, Lawrence D.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Government Document Book

12

Experimental investigation of generic three-dimensional sidewall-compression scramjet inlets at Mach 6 in tetrafluoromethane /

by Holland, Scott D.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993

Book

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