Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow /

Boltz, Frederick W.
United States. National Aeronautics and Space Administration.

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

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).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

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Effects of shock impingement and other factors on leading-edge heat transfer /

Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 10-11).Mode of access: Internet

A comparison of the theoretical and experimental stagnation-point heat transfer in an arc-heated subsonic stream /

Brown, Ronald D.
United States. National Aeronautics and Space Administration.

Cover title."June 1964."Includes bibliographical references (p. 22-23).Mode of access: Internet

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Laminar flow analysis of film boiling from a horizontal wire /

Baumeister, Kenneth J.
Hamill, Thomas D.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 37).Mode of access: Internet

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.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...

Rotational and vibrational temperature measurements in the 12-inch hypersonic ceramic-heated tunnel /

Hoppe, John C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."November 1968."Includes bibliographical references (p. 19-20).Mode of access: Internet

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow /

Boltz, Frederick W.
United States. National Aeronautics and Space Administration.

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

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).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

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Effects of shock impingement and other factors on leading-edge heat transfer /

Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 10-11).Mode of access: Internet

A comparison of the theoretical and experimental stagnation-point heat transfer in an arc-heated subsonic stream /

Brown, Ronald D.
United States. National Aeronautics and Space Administration.

Cover title."June 1964."Includes bibliographical references (p. 22-23).Mode of access: Internet

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Laminar flow analysis of film boiling from a horizontal wire /

Baumeister, Kenneth J.
Hamill, Thomas D.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 37).Mode of access: Internet

Reduction of wind-tunnel wall interference by controlled wall flow /

Bernstein, Samuel.
Joppa, Robert G. (Robert Glenn)
University of Washington. Dept. of Aeronautics and Astronautics.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 47-49).Mode of access: Internet

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover.Includes bibliographical references.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...

Rotational and vibrational temperature measurements in the 12-inch hypersonic ceramic-heated tunnel /

Hoppe, John C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."November 1968."Includes bibliographical references (p. 19-20).Mode of access: Internet

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

Hot-wire heat-loss characteristics and anemometry in subsonic continuum and slip flow /

Boltz, Frederick W.
United States. National Aeronautics and Space Administration.

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

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Abstract

Extracted data

Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flow /

Abstract

Extracted data

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