Search Results

1

Contraction design for small low-speed wind tunnels /

by Bell, J. H.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service, distributor], 1988

Government Document Book

2

Experimental results for a hypersonic nozzle/afterbody flow field /

by Spaid, Frank W.
Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1995

Government Document Book

3

Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1).

Washington, D.C : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book

4

A wind model for an elevated stol-port configuration /

by Peterka, J. A. (Jon A.)
Washington, D.C. : National Aeronautics and Space Administration, 1974

Government Document Book

5

Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel /

by Soderman, Paul T.
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

6

Visualization of leading edge vortices on a series of flat plate delta wings /

by Payne, Francis M.
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, 1991

Government Document Book

7

Full-scale wind-tunnel tests of a small unpowered jet aircraft with a T-Tail /

by Soderman, Paul T.
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

8

Wind-tunnel investigation of a large 35 s̊wept-wing jet transport model with an external-flow jet-augmented double-slotted flap /

by Aoyagi, Kiyoshi
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971

Government Document Book

9

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

10

An experimental investigation of end treatments for nonreturn wind tunnels /

by Eckert, William T., Mort, Kenneth W., Piazza, J. E.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Book

11

Laser-velocimeter surveys of merging vortices in a wind tunnel : complete data and analysis /

by Corsiglia, Victor R., Iversen, James D., Orloff, Kenneth L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

12

Aerodynamic design guidelines and computer program for estimation of subsonic wind tunnel performance /

by Eckert, William T.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

13

Unsteady two dimensional airloads acting on oscillating thin airfoils in subsonic ventilated wind tunnels /

by Fromme, Joseph, Golberg, Michael
Washington : Springfield, Va. : National Aeronautics and Space Adiministration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

14

Two dimensional aerodynamic interference effects on oscillating airfoils with flaps in ventilated subsonic wind tunnels /

by Fromme, Joseph
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book

15

Investigation of the asymmetric aerodynamic characteristics of cylindrical bodies of revolution with variations in nose geometry and rotational orientation at angles of attack to 5...

Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book

16

Crossflow effects on steady and fluctuating pressures on an ogive-cylinder cone-frustum model in supersonic separated flow /

by Dods, Jules B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book

17

Large-scale wind tunnel investigation to improve the low-speed longitudinal stability at high lift of a supersonic transport with variable-sweep wings /

by Cook, Anthony M.
Washington, D.C. : National Aeronautics and Space Administration, 1969

Government Document Book

18

Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport /

by Cook, Anthony M.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document Book

19

Real-time computer data system for the 40- by 80-foot wind-tunnel facility at Ames Research Center /

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

Government Document Book

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