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

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...

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

Experimental study of effects of geometric variables on performance of contoured rocket engine exhaust nozzles /

bloomer, Harry E.
Renas, Paul E.
Antl, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Propulsion system elements; Propulsion systems, liquid-fuel.Includes bibl...

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...

Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles /

Gertsma, Laurence W.
Yeager, Richard A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

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...

Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios /

Reshotko, Eli
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 14, 1953."Title from cover.Includes bibliographical references: p. 19.Mode ...

Thrust-reverser flow investigation on a twin-engine transport /

Gatlin, Gregory M. (Gregory Michael)
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 17).Mode of access: Internet

Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle /

Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

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

Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle /

Johns, Albert L.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

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

January 1980

Dec. 1980."Langely Research Center."Includes bibliographical references.Mode of access: Internet

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

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

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

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...

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

Experimental study of effects of geometric variables on performance of contoured rocket engine exhaust nozzles /

bloomer, Harry E.
Renas, Paul E.
Antl, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Propulsion system elements; Propulsion systems, liquid-fuel.Includes bibl...

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...

Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles /

Gertsma, Laurence W.
Yeager, Richard A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

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...

Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios /

Reshotko, Eli
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 14, 1953."Title from cover.Includes bibliographical references: p. 19.Mode ...

Thrust-reverser flow investigation on a twin-engine transport /

Gatlin, Gregory M. (Gregory Michael)
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 17).Mode of access: Internet

Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle /

Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

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

Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle /

Johns, Albert L.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

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

January 1980

Dec. 1980."Langely Research Center."Includes bibliographical references.Mode of access: Internet

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

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

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

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...

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

Experimental study of effects of geometric variables on performance of contoured rocket engine exhaust nozzles /

bloomer, Harry E.
Renas, Paul E.
Antl, Robert J.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Propulsion system elements; Propulsion systems, liquid-fuel.Includes bibl...

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

Abstract

Extracted data

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

Abstract

Extracted data

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