Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

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...

Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream /

Putnam, Lawrence E. (Lawrence Elwood)
Capone, Francis J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Equivalent solid bodies for representing jet plumes in supersonic stream.Includes bibliographical re...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

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

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN 4 routines

Johnson, R. C.

April 1974

Sets of routines are presented that calculate such real-gas supersonic stream properties as velocity...

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Concentration measurements of an injected gas in a supersonic stream /

Torrence, Marvin G.
Langley Research Center.

Prepared at Langley Research Center."April 1967"--Cover.Includes bibliographical references (p. 11)....

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).Mode of access: Internet

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

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

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 ...

Venting characteristics of gaseous helium and nitrogen discharging into a free stream at Mach numbers from 0.60 to 1.57 /

Johns, Albert L.
Jones, Merle L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 6).Mode of acc...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Calculation of supersonic flows at large distances from slender lifting bodies /

Schorling, M. (Michael)
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodies.Inc...

A method for calculating a real-gas two-dimensional nozzle contour including the effects of gamma /

Johnson, Charles B.
Boney, Lillian R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ...

Numerical calculations for the characteristics of a gas flowing axially through a constricted arc /

Watson, Velvin R. (Velvin Richard)
Pegot, Eva B.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."June 1967"--Cover.Includes bibliographical references (p. 117).Mod...

FORTRAN program for quasi-three-dimensional calculation of surface velocities and choking flow for turbomachine blade rows /

Katsanis, Theodore.

"April 1971."Cover title.Includes bibliographical references (p. 30).Mode of access: Internet

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...

Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream /

Putnam, Lawrence E. (Lawrence Elwood)
Capone, Francis J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Equivalent solid bodies for representing jet plumes in supersonic stream.Includes bibliographical re...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

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

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN 4 routines

Johnson, R. C.

April 1974

Sets of routines are presented that calculate such real-gas supersonic stream properties as velocity...

Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /

Biringen, Sedat.
McMillan, Oden J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"March 1980"--Cover.Includes bibliographical references.Mode of access: Internet

Concentration measurements of an injected gas in a supersonic stream /

Torrence, Marvin G.
Langley Research Center.

Prepared at Langley Research Center."April 1967"--Cover.Includes bibliographical references (p. 11)....

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).Mode of access: Internet

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

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

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 ...

Venting characteristics of gaseous helium and nitrogen discharging into a free stream at Mach numbers from 0.60 to 1.57 /

Johns, Albert L.
Jones, Merle L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 6).Mode of acc...

Computer program for calculating the flow field of supersonic ejector nozzles /

Anderson, Bernhard H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 83).Mode of ac...

Calculation of supersonic flows at large distances from slender lifting bodies /

Schorling, M. (Michael)
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodies.Inc...

A method for calculating a real-gas two-dimensional nozzle contour including the effects of gamma /

Johnson, Charles B.
Boney, Lillian R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 22).Mode of ...

Numerical calculations for the characteristics of a gas flowing axially through a constricted arc /

Watson, Velvin R. (Velvin Richard)
Pegot, Eva B.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."June 1967"--Cover.Includes bibliographical references (p. 117).Mod...

FORTRAN program for quasi-three-dimensional calculation of surface velocities and choking flow for turbomachine blade rows /

Katsanis, Theodore.

"April 1971."Cover title.Includes bibliographical references (p. 30).Mode of access: Internet

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...

Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream /

Putnam, Lawrence E. (Lawrence Elwood)
Capone, Francis J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Equivalent solid bodies for representing jet plumes in supersonic stream.Includes bibliographical re...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

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

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

Abstract

Extracted data

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

Abstract

Extracted data

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