Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

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 ...

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

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

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

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)....

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).Mode of access: Internet

High-speed computing machine calculation of supersonic axisymmetric flows /

Clark, Martha W.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"Department of the Army Project No. 503-06-002; Ordnance Research and Development Project No. TB3-00...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

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

A method for computing supersonic flow around blunt bodies, accompanied by a detached shock wave /

Gilinskiĭ, S. M.
Tini︠a︡kov, G. P.
Telenin, G. F. (Georgiĭ Fedorovich)

"February 1965"--cover."Translation of 'Metod rascheta sverkhzvukovogo obtekaniya zatuplennykh tel s...

A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases /

Chaussee, D. S.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"February 1980"--Cover.Includes Bibliographical reference.Mode of access: Internet

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...

Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones /

Briggs, Benjamin R.
Ames Research Center.

January 1959

"NASA TN D-24.""Ames Research Center, Moffett Field, Calif.""August 1959."Title from cover.Includes ...

A technique for studying interactions between a supersonic body and blast waves approaching obliquely /

Damkevala, Rusi Jal, 1939-., author.
Zumwalt, Glen W., author.
U.S. Atomic Energy Commission.
Sandia Corporation.

"May 1967."Includes bibliographical references (pages 119-122).Mode of access: Internet

Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies /

Hamilton, H. Harris.
Graves, Randolph A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 02."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Calculation of flow fields from bow wave profiles for the downstrream region of blunt-nosed circular cylinders in axial hypersonic flight /

Seiff, Alvin
Whiting, Ellis E.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Mathematics....

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 ...

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

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

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

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)....

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).Mode of access: Internet

High-speed computing machine calculation of supersonic axisymmetric flows /

Clark, Martha W.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"Department of the Army Project No. 503-06-002; Ordnance Research and Development Project No. TB3-00...

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

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

A method for computing supersonic flow around blunt bodies, accompanied by a detached shock wave /

Gilinskiĭ, S. M.
Tini︠a︡kov, G. P.
Telenin, G. F. (Georgiĭ Fedorovich)

"February 1965"--cover."Translation of 'Metod rascheta sverkhzvukovogo obtekaniya zatuplennykh tel s...

A supersonic three-dimensional code for flow over blunt bodies : program documentation and test cases /

Chaussee, D. S.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"February 1980"--Cover.Includes Bibliographical reference.Mode of access: Internet

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...

Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones /

Briggs, Benjamin R.
Ames Research Center.

January 1959

"NASA TN D-24.""Ames Research Center, Moffett Field, Calif.""August 1959."Title from cover.Includes ...

A technique for studying interactions between a supersonic body and blast waves approaching obliquely /

Damkevala, Rusi Jal, 1939-., author.
Zumwalt, Glen W., author.
U.S. Atomic Energy Commission.
Sandia Corporation.

"May 1967."Includes bibliographical references (pages 119-122).Mode of access: Internet

Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies /

Hamilton, H. Harris.
Graves, Randolph A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 02."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Calculation of flow fields from bow wave profiles for the downstrream region of blunt-nosed circular cylinders in axial hypersonic flight /

Seiff, Alvin
Whiting, Ellis E.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Mathematics....

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 ...

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

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

Abstract

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Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

Abstract

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