Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes /

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude /

Straight, David M.
Cullom, Richard R.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"June 1983"--Cover.STAR category 07.Distributed to depository libraries in microfiche."Lewis Researc...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

Mason, Mary L.
Berrier, Bobby L.

May 1988

An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel t...

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

Leavitt, Laurence D.
Re, Richard J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."Langley Research Center.""June 1982"--Cover.Includes bibliographical references...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities /

Wing, David J.
Asbury, Scott C.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 10-11).Mode of access: I...

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

Re, Richard J.
Leavitt, Laurence D.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability /

Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 10-11.Mode of access: Internet

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

Leavitt, Laurence D.
Burley, James R.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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

Re, Richard J.
Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring /

Bare, E. Ann.
Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1987

"July 1987"--Cover.Includes bibliographical references (p. 11-12).Mode of access: Internet

Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft /

Re, Richard J.
Carson, George T.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 11.Mode of access: Internet

An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack /

Capone, Francis J.
Leavitt, Laurence D.
Mason, Mary L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring /

Berrier, Bobby L.
Taylor, John G. (John Gilbert)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 9-10.Mode of access: Internet

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes

Mason, Mary L.
Berrier, Bobby L.

May 1988

A static test was conducted in the static test facility of the Langley 16 ft Transonic Tunnel to eva...

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude /

Straight, David M.
Cullom, Richard R.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"June 1983"--Cover.STAR category 07.Distributed to depository libraries in microfiche."Lewis Researc...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

Mason, Mary L.
Berrier, Bobby L.

May 1988

An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel t...

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

Leavitt, Laurence D.
Re, Richard J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."Langley Research Center.""June 1982"--Cover.Includes bibliographical references...

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities /

Wing, David J.
Asbury, Scott C.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 10-11).Mode of access: I...

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

Re, Richard J.
Leavitt, Laurence D.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability /

Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 10-11.Mode of access: Internet

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

Leavitt, Laurence D.
Burley, James R.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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

Re, Richard J.
Leavitt, Laurence D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring /

Bare, E. Ann.
Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1987

"July 1987"--Cover.Includes bibliographical references (p. 11-12).Mode of access: Internet

Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft /

Re, Richard J.
Carson, George T.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 11.Mode of access: Internet

An experimental investigation of thrust vectoring two-dimensional covergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack /

Capone, Francis J.
Leavitt, Laurence D.
Mason, Mary L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring /

Berrier, Bobby L.
Taylor, John G. (John Gilbert)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 9-10.Mode of access: Internet

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes

Mason, Mary L.
Berrier, Bobby L.

May 1988

A static test was conducted in the static test facility of the Langley 16 ft Transonic Tunnel to eva...

Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude /

Straight, David M.
Cullom, Richard R.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"June 1983"--Cover.STAR category 07.Distributed to depository libraries in microfiche."Lewis Researc...

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring

Mason, Mary L.
Berrier, Bobby L.

May 1988

An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel t...

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

Leavitt, Laurence D.
Re, Richard J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."Langley Research Center.""June 1982"--Cover.Includes bibliographical references...

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes /

Abstract

Extracted data

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes /

Abstract

Extracted data

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