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

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

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...

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle /

Mason, Mary L.
Asbury, Scott C.
Capone, Francis J.
Langley Research Center.

January 1992

Prepared at Langley Research Center."June 1992"--Cover.Includes bibliographical references (p. 9).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...

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 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 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...

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 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 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 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...

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle /

Carson, George T.
Burley, James R.
Bare, E. Ann.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

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...

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle /

Mason, Mary L.
Asbury, Scott C.
Capone, Francis J.
Langley Research Center.

January 1992

Prepared at Langley Research Center."June 1992"--Cover.Includes bibliographical references (p. 9).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...

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 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 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...

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 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 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 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...

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle /

Carson, George T.
Burley, James R.
Bare, E. Ann.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds /

Henderson, William P.
Burley, James R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."November 1987"--Cover.Includes bibliographical references (p. 7...

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...

A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle /

Mason, Mary L.
Asbury, Scott C.
Capone, Francis J.
Langley Research Center.

January 1992

Prepared at Langley Research Center."June 1992"--Cover.Includes bibliographical references (p. 9).Mo...

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

Abstract

Extracted data

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

Abstract

Extracted data

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