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1

High speed aerodynamics and jet propulsion .

Princeton, N. J. : Princeton University Press, 1950

Serial

2

Wing theory in supersonic flow /

by Carafoli, Elie
Oxford, New York : Pergamon Press, 1969
[First edition].

Book

3

High speed aerodynamics and jet propulsion.

Princeton, N.J. : Princeton University Press, 1955

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Serial

4

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

by McMillin, S. Naomi (Susan Naomi)
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book

5

Effect of interjet spacing on mixing of multiple coaxial jets in supersonic flow /

by Lorber, A. K. (Azriel Karol G.), 1935-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

6

Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design /

by Carlson, Harry W.
[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

7

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

by Hingst, Warren R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

8

Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream /

by McClinton, Charles R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

9

Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction /

by Shaw, Robert J. (Robert Joseph), 1946-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1974

Government Document Book

10

Acoustic properties of a supersonic fan /

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

Government Document Book

11

Supersonic aerodynamics of delta wings /

by Wood, Richard M.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988

Government Document Book

12

Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

by Wasserbauer, Joseph F.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

13

Experimental evaluation of a Mach 3.5 axisymmetric inlet /

by Syberg, J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

14

A second order slender wing theory for wings with leading edge separation in supersonic flow /

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

Government Document Book

15

Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration /

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

Book

16

Forward-slanted slot throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction /

by Shaw, Robert J. (Robert Joseph), 1946-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

17

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

by Covell, Peter F.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Government Document Book

18

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

by Wood, Richard M.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1987

Government Document Book

19

Investigation, at inlet locations, of fuselage flow fields at transonic and supersonic speeds /

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

Government Document Book

20

Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream /

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

Government Document Book

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