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

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

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...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Heat transfer from high-temperature surfaces to fluids.

Humble, Leroy V.
Grele, Milton, joint author.
Lowdermilk, Warren H., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Flight Propulsion Research Laboratory.

On front cover: "May 21, 1948."Cover title.Includes bibliographical references (p. 14).Mode of acces...

Heat transfer to a sphere with a retrorocket exhausting into a free stream: MAch 2.0 and 0.8

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.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 ...

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

Rarefied-gas couette flow and heat transfer between parallel plates by model sampling /

Perlmutter, Morris.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

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...

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....

Subcooled boiling heat transfer under forced convection in a heated tube

Papell, S. Stephen.
United States. National Aeronautics and Space Administration.

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

Heat-transfer characteristics of several radiator finned-tube configurations /

Sparrow, E. M. (Ephraim M.)
Minkowycz, W. J.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Analysis of radiative heat transfer for large objects at meteoric speeds /

Yoshikawa, Kenneth K.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 84-86).Includes bibliographical refe...

Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures

Einstein, Thomas H.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear...

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

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...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Heat transfer from high-temperature surfaces to fluids.

Humble, Leroy V.
Grele, Milton, joint author.
Lowdermilk, Warren H., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Flight Propulsion Research Laboratory.

On front cover: "May 21, 1948."Cover title.Includes bibliographical references (p. 14).Mode of acces...

Heat transfer to a sphere with a retrorocket exhausting into a free stream: MAch 2.0 and 0.8

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.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 ...

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

Rarefied-gas couette flow and heat transfer between parallel plates by model sampling /

Perlmutter, Morris.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

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...

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....

Subcooled boiling heat transfer under forced convection in a heated tube

Papell, S. Stephen.
United States. National Aeronautics and Space Administration.

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

Heat-transfer characteristics of several radiator finned-tube configurations /

Sparrow, E. M. (Ephraim M.)
Minkowycz, W. J.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Analysis of radiative heat transfer for large objects at meteoric speeds /

Yoshikawa, Kenneth K.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 84-86).Includes bibliographical refe...

Analysis of heat transfer and pressure drop for a gas flowing through a set of multiple parallel flat plates at high temperatures

Einstein, Thomas H.
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Fluid mechanics; Propulsion system elements; Propulsion systems, nuclear...

Laminar flow transition : a large-eddy simulation /

Biringen, Sedat.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 34."February 1982"--Cover.Includes bibliographical references.Mode of access: Inter...

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...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

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

Abstract

Extracted data

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

Abstract

Extracted data

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