Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. /

Effect of multiple-nozzle geometry on jet noise generation. /

Rollin, Vern G.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Airc...

Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions /

Tuovila, W. J. (Weimer J.)
Land, Norman S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 6).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

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...

Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. /

Lovell, J. Calvin
Samanich, Nick E.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."June 1961."Aerodynamics, missiles and space vehicles; Propulsion system elemen...

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...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

Annular internal-external-expansion rocket nozzles for large booster applications /

Connors, James F.
Mitchell, Glenn A.
Cubbison, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carri...

Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios /

Jones, William L.
Gibb, John W.
Aukerman, Carl A.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 20).Mode of access: Internet

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

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft...

Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins /

Cubbage, James M.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Propulsion system elements.Inc...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket /

Liebert, Curt H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Propellants; Propulsion system elements; Propulsion systems, liquid-fue...

Examination of pressure oscillations induced by changes in the burning rate of flames /

Schalla, Rose L.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Chemistry, physical; Propulsion systems, liquid-fuel rockets; Propulsion sy...

Effect of multiple-nozzle geometry on jet noise generation. /

Rollin, Vern G.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Airc...

Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions /

Tuovila, W. J. (Weimer J.)
Land, Norman S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 6).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

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...

Experimental performance of nozzles having area ratios up to 300 on JP-4 fuel - liquid-oxygen rocket engine. /

Lovell, J. Calvin
Samanich, Nick E.
United States. National Aeronautics and Space Administration.

Abstract:Cover title."June 1961."Aerodynamics, missiles and space vehicles; Propulsion system elemen...

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...

Base flow characteristics for several four-clustered rocket configurations at mach numbers from 2.0 to 3.5 /

Musial, Normal T.
Ward, James J.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Aerodynamics, missiles and space vehicles; Propulsion systems, liquid-fu...

Annular internal-external-expansion rocket nozzles for large booster applications /

Connors, James F.
Mitchell, Glenn A.
Cubbison, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carri...

Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios /

Jones, William L.
Gibb, John W.
Aukerman, Carl A.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 20).Mode of access: Internet

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

The effect of thrust minus base drag of exchanging base area for nozzle expansion in supersonic nozzles at transonic mach numbers /

Slocumb, Travis H.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft...

Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins /

Cubbage, James M.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Propulsion system elements.Inc...

Exploratory tests of the effects of jet plumes on the flow over cone-cylinder-flare bodies /

Falanga, Ralph A.
Crawford, Davis H.
Hinson, William F.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aerodynamics, missiles and space vehicles.Includes bibliographical refer...

Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket /

Liebert, Curt H.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Propellants; Propulsion system elements; Propulsion systems, liquid-fue...

Examination of pressure oscillations induced by changes in the burning rate of flames /

Schalla, Rose L.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Chemistry, physical; Propulsion systems, liquid-fuel rockets; Propulsion sy...

Effect of multiple-nozzle geometry on jet noise generation. /

Rollin, Vern G.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Airc...

Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions /

Tuovila, W. J. (Weimer J.)
Land, Norman S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 6).Mode of access: Internet

An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles /

Gungle, Robert L.
Leonard, H. Wayne.
Brosier, William S.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, missiles and space vehicles;Launching dynamics; Missiles and ...

Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. /

Abstract

Extracted data

Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. /

Abstract

Extracted data

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