Search Results

1

Wind-tunnel investigation at low speeds of a model of the Kestrel (XV-6A) vectored-thrust V/STOL airplane /

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

Government Document Book

2

Review of propulsion-induced effects on aerodynamics of jet/stol aircraft /

by Margason, Richard J. (Richard John), 1936-
Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970

Government Document Book

3

Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model /

by Carter, Arthur W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1969

Government Document Book

4

Low-speed aerodynamic characteristics of a 17-percent-thick airfoil section designed for general aviation applications /

by McGhee, Robert J.
Washington D.C. : Alexandria, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1973

Government Document Book

5

Full-scale wind-tunnel investigation of effects of slot spoilers on the aerodynamic characteristics of a light twin-engine airplane /

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

Government Document Book

6

Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with so...

by Wells, William R.
Washington, D.C. : U.S. G.P.O., 1962

Government Document Book

7

Experimental static aerodynamics of a regular hexagonal prism in a low-density hypervelocity flow /

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

Government Document Book

8

Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow /

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

Government Document Book

9

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

10

Analytical study of effects of severe turbulence on flight motions of a typical subsonic jet-transport airplane /

by Grantham, William D.
Washington, D.C. : National Aeronautics and Space Administration, 1969

Government Document Book

11

Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds /

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

Government Document Book

12

Stagnation-point shielding by melting and vaporization /

by Roberts, Leonard
Washington, DC : U.S. G.P.O., 1959

Government Document Book

13

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

14

Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

by Winston, Matthew M.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1969

Government Document Book

15

Calculation of aerodynamic loading and twist characteristics of a flexible wing at Mach numbers approaching 1.0 and comparison with experiment /

by Mugler, John P.
Washington, D.C. : Springfield, VA : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960

Government Document Book

16

Measured vibration response characteristics of four residential structures excited by mechanical and acoustical loadings /

by Carden, Huey P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [Available through the Clearinghouse for Federal Scientific and Technical Information], 1970

Government Document Book

17

Effect of engine position and high-lift devices on aerodynamic characteristics of an external-flow jet-flap STOL model /

by Smith, Charles C., Jr
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1971

Government Document Book

18

A Theoretical study of stagnation-point ablation /

by Roberts, Leonard
Washington, DC : U.S. G.P.O., 1959

Government Document Book

19

Atomization, drop size, and penetration for cross-stream water injection at high-altitude reentry conditions with application to the RAM C-I and C-III flights /

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

Government Document Book

20

Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V/STOL model in transition /

by Winston, Matthew M.
Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970

Government Document Book

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