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1

Hypersonic and transonic buzz measurements on the lower pitch flap of M2-F2 lifting entry configuration /

by Warner, Robert W. (Robert William)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

2

Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 /

by Kemp, Joseph H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

3

The use of self-calibrating catalytic probes to measure free-stream atom concentration in a hypersonic flow /

by Reddy, N. M.
Washington, D.C. : National Aeronautics and Space Administration, 1967

Government Document Book

4

The Rotornet : a high performance hypersonic decelerator for planetary entry /

by Kyser, A. C.
Washington, D.C. : NASA, 1965

Government Document Book

5

Effect of bluntness on hypersonic two-dimensional inlet type flows /

by Sanator, Robert J.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document Book

6

Experimental aerodynamic characteristics of 10 short axisymmetric bodies at Mach numbers of 5 to 15 /

by Chapman, Gary T.
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965

Government Document Book

7

Pilot model expansion tunnel test flow properties obtained from velocity, pressure, and probe measurements /

by Friesen, Wilfred J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

8

Analysis of hypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers /

by Nagel, A. L.
[Washington, D.C.] : National Aeronautics and Space Administration, 1966

Government Document Book

9

NSEG : a segmented mission analysis program for low and high speed aircraft /

by Hague, D. S.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

10

Hypersonic rarefied flow over sharp slender cones /

by Kussoy, M. I. (Marvin I.)
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972

Government Document Book

11

Measured and calculated mean-flow properties of a two-dimensional, hypersonic, turbulent wake /

by Wagner, Richard D. (Richard Dirk), 1936-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

12

Starting phenomena for hypersonic inlets with thick turbulent boundary layers at Mach 6 /

by Goldberg, Theodore J.
Washington, D.C. : Springfield, VA : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971

Government Document Book

13

Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel /

by Hiers, Robert Smith, 1936-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969

Government Document Book

14

Discrete sonic jets used as boundary-layer trips at Mach numbers of 6 and 8.5 /

by Stone, David R. (David Ray)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

15

Use of tetrafluoromethane to simulate real-gas effects on the hypersonic aerodynamics of blunt vehicles /

by Jones, Robert A.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969

Government Document Book

16

A technique for measuring hypersonic flow velocity profiles /

by Gartrell, Luther R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

17

Aerodynamic and flow-visualization studies of two delta-wing entry vehicles at a Mach number of 20.3 /

by Arrington, James P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

18

Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 /

by Weinstein, Irving
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

19

Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 /

by Nelms, Walter P.
Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971

Government Document Book

20

Analysis of the flow in a 1-MJ electric-arc shock tunnel /

by Reller, John O.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

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