Methods of predicting laminar heat rates on hypersonic vehicles /

Heat transfer in laminar flows of incompressible fluids with Pr - zero and Pr - infinity

Adams, Ernst W.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation /

Schacht, Ralph L.
Quentmeyer, Richard J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Mode of access: Internet

Data-reduction technique for determining rapidly rising heating rates to thermally thick walls /

Dillon, James L.
Smith, G. Louis (George Louis)
Wright, Robert L. (Robert Lewis), 1935-
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."July 1969"--Cover.Includes bibliographical references (p. 14).M...

Laminar skin-friction and heat-transfer parameters for a flat plate at hypersonic speeds in terms of free-stream flow properties /

Schmidt, James F.
Lewis Research Center.

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

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /

Hamilton, H. Harris.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Includes bibliographical references.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....

A simplified method for calculating laminar heat transfer over bodies at an angle of attack /

DeJarnette, Fred R.
Davis, Ruby M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 15).Mode of access: Internet

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 ...

Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams /

Weltmann, Ruth N., 1912-
Kuhns, Perry W.
Lewis Research Center.

Prepared at Lewis Research Center."March 1960."Cover title.Includes bibliographical references (p. 1...

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 (...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

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...

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

Heat transfer in laminar flows of incompressible fluids with Pr - zero and Pr - infinity

Adams, Ernst W.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation /

Schacht, Ralph L.
Quentmeyer, Richard J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Mode of access: Internet

Data-reduction technique for determining rapidly rising heating rates to thermally thick walls /

Dillon, James L.
Smith, G. Louis (George Louis)
Wright, Robert L. (Robert Lewis), 1935-
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."July 1969"--Cover.Includes bibliographical references (p. 14).M...

Laminar skin-friction and heat-transfer parameters for a flat plate at hypersonic speeds in terms of free-stream flow properties /

Schmidt, James F.
Lewis Research Center.

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

Numerical computation of aerodynamic heating of liquid propellants /

Kramer, John L.
Roudebush, William H.
Lowell, Herman H.
Lewis Research Center.

Prepared at Lewis Research Center."April 1960."Cover title.Includes bibliographical references (p. 1...

Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /

Hamilton, H. Harris.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Includes bibliographical references.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....

A simplified method for calculating laminar heat transfer over bodies at an angle of attack /

DeJarnette, Fred R.
Davis, Ruby M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 15).Mode of access: Internet

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 ...

Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams /

Weltmann, Ruth N., 1912-
Kuhns, Perry W.
Lewis Research Center.

Prepared at Lewis Research Center."March 1960."Cover title.Includes bibliographical references (p. 1...

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 (...

Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. /

Wagner, Richard D.
Henderson, Arthur, 1922-
Pine, W. Clint.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogr...

Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

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...

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

Heat transfer in laminar flows of incompressible fluids with Pr - zero and Pr - infinity

Adams, Ernst W.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation /

Schacht, Ralph L.
Quentmeyer, Richard J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Mode of access: Internet

Data-reduction technique for determining rapidly rising heating rates to thermally thick walls /

Dillon, James L.
Smith, G. Louis (George Louis)
Wright, Robert L. (Robert Lewis), 1935-
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."July 1969"--Cover.Includes bibliographical references (p. 14).M...

Methods of predicting laminar heat rates on hypersonic vehicles /

Abstract

Extracted data

Methods of predicting laminar heat rates on hypersonic vehicles /

Abstract

Extracted data

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