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 /

Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. /

Henderson, Arthur, 1922-
Braswell, Dorothy O.
United States. National Aeronautics and Space Administration.

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

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 /

Siler, L. G., author.
Deskins, H. E., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"November 1964."Includes bibliographic references (page 5).Report prepared by ARO, Inc., under Air F...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

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

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...

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.

Becker, John V.
Korycinski, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

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...

Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 /

Stallings, Jr., Robert L.
Burbank, Paige B.
Langley Research Center.

January 1959

"October 1959"--Cover.Caption title.Includes bibliographical references (p. 10).Mode of access: Inte...

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...

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...

Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Monta, William J.
United States. National Aeronautics and Space Administration.

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

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

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...

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. /

Henderson, Arthur, 1922-
Braswell, Dorothy O.
United States. National Aeronautics and Space Administration.

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

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 /

Siler, L. G., author.
Deskins, H. E., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"November 1964."Includes bibliographic references (page 5).Report prepared by ARO, Inc., under Air F...

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

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

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...

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.

Becker, John V.
Korycinski, Peter F.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliog...

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...

Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 /

Stallings, Jr., Robert L.
Burbank, Paige B.
Langley Research Center.

January 1959

"October 1959"--Cover.Caption title.Includes bibliographical references (p. 10).Mode of access: Inte...

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...

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...

Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Monta, William J.
United States. National Aeronautics and Space Administration.

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

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

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...

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. /

Henderson, Arthur, 1922-
Braswell, Dorothy O.
United States. National Aeronautics and Space Administration.

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

Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 /

Peterson, Victor L.
McKenzie, Robert L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry; Fluid mechanics...

Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds /

Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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