A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 /

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

A method for predicting shock shapes and pressure distributions for a wide variety of blunt bodies at zero angle of attack /

Kaattari, George E.
Ames Research Center.

Prepared at Ames Research Center."April 1968"--Cover.Includes bibliographical references (p. 41).Mod...

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and CO₂ flows, and calibration results in Langley 6-inch expansion tube /

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

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 31-33).Mode ...

Pressures, forces and moments, and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in helium /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"January 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds /

Jernell, Lloyd S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Shock-wave shapes and surface pressures on hemisphere- and cone-cylinders in low-density hypersonic flow including ablation /

Monson, Daryl J.
Kuehn, Donald M.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Also available online.Includes bibliographical references (p. 12-13).Also available online.Mode of a...

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

Theoretical prediction of pressures in hypersonic flow with special reference to configurations having attached leading-edge shock.

Scheuing, Richard A., author.
Melnik, Robert E., author.
Brook, John W., author.
Mead, Harold R., author.
Aeronautical Research Associates of Princeton. sponsor.
Grumman Aircraft Engineering Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body.
United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor.
United States. Aerospace Medical Division. sponsor.

"May 1962."Includes bibliographical references (pages 174-177).Flight Control Laboratory Contract No...

Comparison of jet plume shape predictions and plume influence on sonic boom signature /

Barger, Raymond L.
Melson, N. Duane.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 4).Mode of access: Inter...

A theoretical and experimental study of hypersonic flow over flared bodies at incidence /

Rakich, John V.
Menees, Gene P.
Ames Research Center.

Prepared at Ames Research Center."January 1966"--Cover.Includes bibliographical references (p. 29-30...

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19

Miller, C. G., III

December 1975

Measured shock shapes are presented for sphere and hemisphere models in helium, air, CF4, C2F6, and ...

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

A method for predicting shock shapes and pressure distributions for a wide variety of blunt bodies at zero angle of attack /

Kaattari, George E.
Ames Research Center.

Prepared at Ames Research Center."April 1968"--Cover.Includes bibliographical references (p. 41).Mod...

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and CO₂ flows, and calibration results in Langley 6-inch expansion tube /

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

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 31-33).Mode ...

Pressures, forces and moments, and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in helium /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"January 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds /

Jernell, Lloyd S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Shock-wave shapes and surface pressures on hemisphere- and cone-cylinders in low-density hypersonic flow including ablation /

Monson, Daryl J.
Kuehn, Donald M.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Also available online.Includes bibliographical references (p. 12-13).Also available online.Mode of a...

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

Theoretical prediction of pressures in hypersonic flow with special reference to configurations having attached leading-edge shock.

Scheuing, Richard A., author.
Melnik, Robert E., author.
Brook, John W., author.
Mead, Harold R., author.
Aeronautical Research Associates of Princeton. sponsor.
Grumman Aircraft Engineering Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body.
United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor.
United States. Aerospace Medical Division. sponsor.

"May 1962."Includes bibliographical references (pages 174-177).Flight Control Laboratory Contract No...

Comparison of jet plume shape predictions and plume influence on sonic boom signature /

Barger, Raymond L.
Melson, N. Duane.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 4).Mode of access: Inter...

A theoretical and experimental study of hypersonic flow over flared bodies at incidence /

Rakich, John V.
Menees, Gene P.
Ames Research Center.

Prepared at Ames Research Center."January 1966"--Cover.Includes bibliographical references (p. 29-30...

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19

Miller, C. G., III

December 1975

Measured shock shapes are presented for sphere and hemisphere models in helium, air, CF4, C2F6, and ...

A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack /

Kaattari, George E.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 28.Mode of access: Internet

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

A method for predicting shock shapes and pressure distributions for a wide variety of blunt bodies at zero angle of attack /

Kaattari, George E.
Ames Research Center.

Prepared at Ames Research Center."April 1968"--Cover.Includes bibliographical references (p. 41).Mod...

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 /

Abstract

Extracted data

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 /

Abstract

Extracted data

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