Numerical computation of aerodynamic heating of liquid propellants /

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow /

Beckwith, Ivan E.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

Methods of predicting laminar heat rates on hypersonic vehicles /

Wisniewski, Richard J.
Lewis Research Center.

Prepared at Lewis Research Center."December 1959."Cover title.Includes bibliographical references (p...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Some observations of base heating at Mach 3.0 on a simulated missile with JP-4 liquid-oxygen rocket /

Samanich, Nick E.
Barnett, Donald D.
Lovell, J. Calvin.
Lewis Research Center.

January 1960

"November 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Unsteady stagnation-point heat transfer /

Sparrow, E. M. (Ephraim M.)
Lewis Research Center.

Prepared at Lewis Research Center."October 1959."Cover title.Includes bibliographical references (p....

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...

A radiant heater to simulate aerodynamic heating in a wind tunnel /

Trussell, Donald H.
Weidman, Deene J. (Deene Jon), 1932-
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

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

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 24).M...

Comparison of theoretical and experimental values for the effective heat of ablation of ammonium chloride /

Walker, Jean E.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry; Materials,...

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

Radio-frequency induction heating of low-pressure plasmas /

Sovie, Ronald J.
Seikel, George R.
Lewis Research Center.

Prepared at Lewis Research Center."October 1967"--Cover.Includes bibliographical references (p. 59-6...

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow /

Beckwith, Ivan E.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

Methods of predicting laminar heat rates on hypersonic vehicles /

Wisniewski, Richard J.
Lewis Research Center.

Prepared at Lewis Research Center."December 1959."Cover title.Includes bibliographical references (p...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Some observations of base heating at Mach 3.0 on a simulated missile with JP-4 liquid-oxygen rocket /

Samanich, Nick E.
Barnett, Donald D.
Lovell, J. Calvin.
Lewis Research Center.

January 1960

"November 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Unsteady stagnation-point heat transfer /

Sparrow, E. M. (Ephraim M.)
Lewis Research Center.

Prepared at Lewis Research Center."October 1959."Cover title.Includes bibliographical references (p....

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...

A radiant heater to simulate aerodynamic heating in a wind tunnel /

Trussell, Donald H.
Weidman, Deene J. (Deene Jon), 1932-
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

Experimental and theoretical study of heat conduction for air up to 5000 degrees F /

Peng, Tzy-Cheng.
Ahtye, Warren F.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Chemical engineering; Chemist...

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

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

January 1987

Prepared at Lewis Research Center."August 1987"--Cover.Includes bibliographical references (p. 24).M...

Comparison of theoretical and experimental values for the effective heat of ablation of ammonium chloride /

Walker, Jean E.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, missiles and space vehicles; Atmospheric entry; Materials,...

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

Radio-frequency induction heating of low-pressure plasmas /

Sovie, Ronald J.
Seikel, George R.
Lewis Research Center.

Prepared at Lewis Research Center."October 1967"--Cover.Includes bibliographical references (p. 59-6...

Boiling heat transfer to liquid hydrogen and nitrogen in forced flow /

Lewis, James P.
Kline, John F.
Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Fluid mechanics; Propellants; Propulsion system elements; Propulsion sy...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow /

Beckwith, Ivan E.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

Numerical computation of aerodynamic heating of liquid propellants /

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Numerical computation of aerodynamic heating of liquid propellants /

Abstract

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