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

Effect of geometric parameters on the static performance of an annular nozzle with a concave central base /

Mercer, Charles E.
Simonson, Albert J.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion s...

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Keyes, J. Wayne.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 11).Mo...

Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 /

Maiden, Donald L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 21-22).Mode of access: Internet

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

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

Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /

Berrier, Bobby L.
Re, Richard J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02.Includes statistical tables."July 1979"--Cover."Langley Research Center."Include...

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...

Investigation of installation effects on twin-engine convergent-divergent nozzles /

Bare, E. Ann.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

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 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

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 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 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...

Effect of geometric parameters on the static performance of an annular nozzle with a concave central base /

Mercer, Charles E.
Simonson, Albert J.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion s...

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Keyes, J. Wayne.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 11).Mo...

Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 /

Maiden, Donald L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 21-22).Mode of access: Internet

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

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

Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /

Berrier, Bobby L.
Re, Richard J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02.Includes statistical tables."July 1979"--Cover."Langley Research Center."Include...

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...

Investigation of installation effects on twin-engine convergent-divergent nozzles /

Bare, E. Ann.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

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 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

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 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 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...

Effect of geometric parameters on the static performance of an annular nozzle with a concave central base /

Mercer, Charles E.
Simonson, Albert J.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion s...

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Keyes, J. Wayne.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 11).Mo...

Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 /

Maiden, Donald L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 21-22).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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