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

Internal performance of several divergent-shroud ejector nozzles with high divergence angles /

Trout, Arthur M.
Povolny, John H.
Papell, S. Stephen.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 2, 1957."Includes bibliographical references (p. 21-22).Mode of access: Internet

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...

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 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...

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

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

January 1984

Subject category 02."December 1984"--Cover.Distributed to depository libraries in microfiche.Bibliog...

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 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 investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

Mason, Mary L.
Burley, James R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 13-1...

Internal performance of several divergent-shroud ejector nozzles with high divergence angles /

Trout, Arthur M.
Povolny, John H.
Papell, S. Stephen.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 2, 1957."Includes bibliographical references (p. 21-22).Mode of access: Internet

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...

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 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...

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

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

January 1984

Subject category 02."December 1984"--Cover.Distributed to depository libraries in microfiche.Bibliog...

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 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 investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /

Mason, Mary L.
Burley, James R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 13-1...

Internal performance of several divergent-shroud ejector nozzles with high divergence angles /

Trout, Arthur M.
Povolny, John H.
Papell, S. Stephen.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 2, 1957."Includes bibliographical references (p. 21-22).Mode of access: Internet

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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