Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Aerodynamic heating and boundary-layer transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 X 10(6) /

Garland, Benjamine J.
Speegle, Katherine C.
Swanson, Andrew G.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer.

Ferguson, Harold.
Schaefer, John W.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmosp...

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...

Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 /

Rumsey, Charles R.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

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

Effect of shock impingement on the distribution of heat-transfer coefficients on a right circular cylinder at mach numbers of 2.65, 3.51, and 4.44 /

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

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

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 ...

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Heat-transfer and pressure measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at mach numbers of 2.65, 3.51, and 4.44 / Paige B. Burbank, Robert A. Newlander and Ida K. Collins.

Burbank, Paige B.
Collins, Ida K.
Newlander, Robert A.
United States. National Aeronautics and Space Administration.

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

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Aerodynamic heating and boundary-layer transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 X 10(6) /

Garland, Benjamine J.
Speegle, Katherine C.
Swanson, Andrew G.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

Heat transfer and pressure distribution on cone-cylinder-flare configuration with boundary-layer separation / Harold Ferguson and John W. Schaefer.

Ferguson, Harold.
Schaefer, John W.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Atmosp...

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...

Measurements of aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in free flight at mach numbers up to 4.7 /

Rumsey, Charles R.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

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

Effect of shock impingement on the distribution of heat-transfer coefficients on a right circular cylinder at mach numbers of 2.65, 3.51, and 4.44 /

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

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

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 ...

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Heat-transfer and pressure measurements on a flat-plate surface and heat-transfer measurements on attached protuberances in a supersonic turbulent boundary layer at mach numbers of 2.65, 3.51, and 4.44 / Paige B. Burbank, Robert A. Newlander and Ida K. Collins.

Burbank, Paige B.
Collins, Ida K.
Newlander, Robert A.
United States. National Aeronautics and Space Administration.

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

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Aerodynamic heating and boundary-layer transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up to 16 X 10(6) /

Garland, Benjamine J.
Speegle, Katherine C.
Swanson, Andrew G.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

Theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body /

Swann, Robert T.
South, Jerry C. (Jerry Curtis), 1935-
United States. National Aeronautics and Space Administration.

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

Local aerodynamic heat transfer and boundary-layer transition on roughened sphere-ellipsoid bodies at mach number 3.0/

Deveikis, William D.
Walker, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Fluid...

Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Abstract

Extracted data

Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski.

Abstract

Extracted data

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