Search Results

1

Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60° /

by Leavitt, Laurence D.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Government Document Book

2

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities /

by Leavitt, Laurence D.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985

Government Document Book

3

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /

by Re, Richard J.
[Washington, D.C.] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986

Government Document Book

4

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /

by Yetter, Jeffery A.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

5

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45° /

by Henderson, William P.
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

6

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics /

by Leavitt, Laurence D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

7

Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2 /

by Leavitt, Laurence D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

8

Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters /

by Re, Richard J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book

9

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

by Leavitt, Laurence D.
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

10

Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles /

by Leavitt, Laurence D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book

11

Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles /

by Re, Richard J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book

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