Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions /

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

Numerical solutions of the Navier-Stokes equations for the supersonic laminar flow over a two-dimensional compression corner /

Carter, James E. (James Edward), 1944-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 76-79).Mode ...

Steady subsonic flow around finite-thickness wings /

Kuo, Ching-Chiang.
Morino, L.
Langley Research Center.
Boston University. Dept. of Aerospace Engineering.

"Prepared by Boston University, [Dept. of Aerospace Engineering] ... for Langley Research Center.""N...

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

McMillin, S. Naomi (Susan Naomi)
Murman, Earll M., 1942-
Thomas, James L. (James Lee), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 98-99.Mode of access: Internet

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Development of upwind schemes for the Euler equations /

Chakravarthy, Sukumar R. (Sukumar Raman)
Langley Research Center.

January 1987

"January 1987"--Cover."Prepared for Langley Research Center under contract NAS1-17492."Includes bibl...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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...

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊/

Mascitti, Vincent R. (Vincent Robert), 1941-
Langley Research Center.

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).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 ...

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

Numerical solutions of the Navier-Stokes equations for the supersonic laminar flow over a two-dimensional compression corner /

Carter, James E. (James Edward), 1944-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 76-79).Mode ...

Steady subsonic flow around finite-thickness wings /

Kuo, Ching-Chiang.
Morino, L.
Langley Research Center.
Boston University. Dept. of Aerospace Engineering.

"Prepared by Boston University, [Dept. of Aerospace Engineering] ... for Langley Research Center.""N...

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment /

McMillin, S. Naomi (Susan Naomi)
Murman, Earll M., 1942-
Thomas, James L. (James Lee), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 98-99.Mode of access: Internet

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Development of upwind schemes for the Euler equations /

Chakravarthy, Sukumar R. (Sukumar Raman)
Langley Research Center.

January 1987

"January 1987"--Cover."Prepared for Langley Research Center under contract NAS1-17492."Includes bibl...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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...

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊/

Mascitti, Vincent R. (Vincent Robert), 1941-
Langley Research Center.

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).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 ...

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions /

Abstract

Extracted data

Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions /

Abstract

Extracted data

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