Study of the nonequilibrium flow field behind normal shock waves in carbon dioxide /

Local stability analysis for a planar shock wave /

Salas, M. D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Shock-tube flow analysis with a dimensionless velocity number /

Reddy, N. Muniswamy.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Shock tube flow analysis with dimensionless velocity number.Prepared at Ames Research Center."Novemb...

Investigation of the mixing and combustion of turbulent, compressible free jets /

Cohen, Leonard S.
Guile, Roy N.
United Aircraft Corporation. Research Laboratories.

"December 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Thermodynamic properties of carbon-dioxide and nitrogen mixtures behind a normal shock wave /

Woodward, Henry T.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."March 1963"--Cover.Includes bibliographical references (p. 6).Mode...

A simplified study on the nonequilibrium Couette and boundary-layer flows with air injection /

Chung, Paul M. (Paul Myung-Ha)
Ames Research Center.

Prepared at Ames Research Center."February 1960."Cover title.Includes bibliographical references (p....

An estimate of the chemical kinetics behind normal shock waves in mixtures of carbon dioxide and nitrogen for conditions of Mars entry /

McKenzie, Robert L.
Ames Research Center.

Prepared at Ames Research Center."February 1966"--Cover.Includes bibliographical references (p. 23-2...

Radiative heat transfer and absorption behind a hypersonic normal shock wave /

Yoshikawa, Kenneth K.
Chapman, Dean R.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

On the direct solution of the governing equation for radiation-resisted shock waves /

Pearson, Walter E.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel [electronic resource] /

Hiers, Robert Smith, 1936-
Reller, John O.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."January 1969"--Cover.Includes bibliographical references (p. 16-17...

Carbon dioxide dissociation rates behind shock waves /

Steinberg, Michel.
General Motors Corporation.
United States. National Aeronautics and Space Administration.

"February 1965." --- cover.Bibliography: p. 25-24.Prepared by General Motors Corporation, Santa Barb...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

Investigations of the interaction of boundary layer and shock waves in transonic flow /

Liepmann, H. W. (Hans Wolfgang), 1914-2009, author.
Platt, Jospeh, author.
Goppert, Jean G., author.
California Institute of Technology, sponsor.
United States. Air Force. Air Matériel Command, issuing body.

Report prepared by the California Institute of Technology, Pasadena, California."9 February 1948."In...

An investigation of resonant, nonlinear, nonplanar free surface oscillations of a fluid /

Hutton, R. E.
United States. National Aeronautics and Space Administration.

Cover title."May 1963."Includes bibliographical references.Mode of access: Internet

Predicted gas properties in the shock layer ahead of capsule-type vehicles at angles of attack /

Kaattari, George E.
Ames Research Center.

Prepared at Ames Research Center."October 1962."Cover title.Includes bibliographical references (p. ...

Local stability analysis for a planar shock wave /

Salas, M. D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Shock-tube flow analysis with a dimensionless velocity number /

Reddy, N. Muniswamy.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Shock tube flow analysis with dimensionless velocity number.Prepared at Ames Research Center."Novemb...

Investigation of the mixing and combustion of turbulent, compressible free jets /

Cohen, Leonard S.
Guile, Roy N.
United Aircraft Corporation. Research Laboratories.

"December 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Thermodynamic properties of carbon-dioxide and nitrogen mixtures behind a normal shock wave /

Woodward, Henry T.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."March 1963"--Cover.Includes bibliographical references (p. 6).Mode...

A simplified study on the nonequilibrium Couette and boundary-layer flows with air injection /

Chung, Paul M. (Paul Myung-Ha)
Ames Research Center.

Prepared at Ames Research Center."February 1960."Cover title.Includes bibliographical references (p....

An estimate of the chemical kinetics behind normal shock waves in mixtures of carbon dioxide and nitrogen for conditions of Mars entry /

McKenzie, Robert L.
Ames Research Center.

Prepared at Ames Research Center."February 1966"--Cover.Includes bibliographical references (p. 23-2...

Radiative heat transfer and absorption behind a hypersonic normal shock wave /

Yoshikawa, Kenneth K.
Chapman, Dean R.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

On the direct solution of the governing equation for radiation-resisted shock waves /

Pearson, Walter E.
Ames Research Center.

Prepared at Ames Research Center."January 1964"--Cover.Includes bibliographical references (p. 13).M...

Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel [electronic resource] /

Hiers, Robert Smith, 1936-
Reller, John O.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."January 1969"--Cover.Includes bibliographical references (p. 16-17...

Carbon dioxide dissociation rates behind shock waves /

Steinberg, Michel.
General Motors Corporation.
United States. National Aeronautics and Space Administration.

"February 1965." --- cover.Bibliography: p. 25-24.Prepared by General Motors Corporation, Santa Barb...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

Investigations of the interaction of boundary layer and shock waves in transonic flow /

Liepmann, H. W. (Hans Wolfgang), 1914-2009, author.
Platt, Jospeh, author.
Goppert, Jean G., author.
California Institute of Technology, sponsor.
United States. Air Force. Air Matériel Command, issuing body.

Report prepared by the California Institute of Technology, Pasadena, California."9 February 1948."In...

An investigation of resonant, nonlinear, nonplanar free surface oscillations of a fluid /

Hutton, R. E.
United States. National Aeronautics and Space Administration.

Cover title."May 1963."Includes bibliographical references.Mode of access: Internet

Predicted gas properties in the shock layer ahead of capsule-type vehicles at angles of attack /

Kaattari, George E.
Ames Research Center.

Prepared at Ames Research Center."October 1962."Cover title.Includes bibliographical references (p. ...

Local stability analysis for a planar shock wave /

Salas, M. D.
Langley Research Center.

January 1984

Prepared at Langley Research Center."December 1984"--Cover.Includes bibliographical references (p. 1...

Shock-tube flow analysis with a dimensionless velocity number /

Reddy, N. Muniswamy.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Shock tube flow analysis with dimensionless velocity number.Prepared at Ames Research Center."Novemb...

Investigation of the mixing and combustion of turbulent, compressible free jets /

Cohen, Leonard S.
Guile, Roy N.
United Aircraft Corporation. Research Laboratories.

"December 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Study of the nonequilibrium flow field behind normal shock waves in carbon dioxide /

Abstract

Extracted data

Study of the nonequilibrium flow field behind normal shock waves in carbon dioxide /

Abstract

Extracted data

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