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

Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 /

Stofan, Andrew J.
Mihaloew, James R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1961

"January 1961."Cover title.Includes bibliographical references (p. 7).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...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

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 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...

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps /

Leavitt, Lawrence D.
Bangert, Linda S.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 /

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

January 1984

Subject category 02.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

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 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...

Thrust performance of a variable-geometry, divergent exhaust nozzle on a turbojet engine at altitude

Straight, D. M.
Collom, R. R.

June 1983

A variable geometry, low aspect ratio, nonaxisymmetric, two dimensional, convergent-divergent exhaus...

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

Foley, Robert J.
Pendergraft, Odis C.
Langley Research Center.

January 1991

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

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...

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...

Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 /

Stofan, Andrew J.
Mihaloew, James R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1961

"January 1961."Cover title.Includes bibliographical references (p. 7).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...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

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 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...

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps /

Leavitt, Lawrence D.
Bangert, Linda S.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 /

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

January 1984

Subject category 02.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

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 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...

Thrust performance of a variable-geometry, divergent exhaust nozzle on a turbojet engine at altitude

Straight, D. M.
Collom, R. R.

June 1983

A variable geometry, low aspect ratio, nonaxisymmetric, two dimensional, convergent-divergent exhaus...

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

Foley, Robert J.
Pendergraft, Odis C.
Langley Research Center.

January 1991

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

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...

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...

Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 /

Stofan, Andrew J.
Mihaloew, James R.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1961

"January 1961."Cover title.Includes bibliographical references (p. 7).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...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

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

Abstract

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

Abstract

Extracted data

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