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

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

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 description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies

Inouye, M.
Rakich, J. V.
Lomax, H.

August 1965

Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...

Application of a numerical orthogonal coordinate generator to axisymmetric blunt bodies /

Graves, Randolph A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 64."October 1979"--Cover."Langley Research Center."Includes bibliographical referen...

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

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...

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 /

Carson, George T.
Lee, Edwin E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"December 1981"--Cover."Langley Research Center."Includes bibiliographical references.Mode of access...

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 method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body /

Suttles, John T. (John Timothy)
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

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...

Computation of equilibrium hypersonic flow about blunt axisymmetric bodies with sharp concers : (Final Report) /

Curtis, J. T., author.
Strom, C. R., author.
Sandia Corporation
U.S. Atomic Energy Commission.

"Purchase Orders 4804, Suborder 10 and 5003, Suborder 9.""August 1967."Includes bibliographical refe...

Calculation of axisymmetric laminar supersonic flow over blunt bodies

Mueller, B.
Oertel, H.
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V. (DFVLR), Goettingen (Germany). Aerodynamische Versuchsanstalt
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V. (DFVLR), Goettingen (Germany). Inst. fuer Theoretische Stroemungsmechanik

January 1984

SIGLETIB: RN 9843 (84A02) / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische Informations...

Three-dimensional inviscid flow about supersonic blunt cones at angle of attack.

Moretti, G., author.
U.S. Atomic Energy Commission.
General Applied Science Laboratories (Westbury, Nassau County, N.Y.)
Sandia Corporation.

Comparisons are made between the cylindrical and polar coordinate system used in determining the thr...

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 ...

Viscous compressible flow about blunt bodies using a numerically generated orthogonal coordinate system

Hamilton, H. H., II
Graves, R. A., Jr.

July 1980

A numerical solution to the Navier-Stokes equations was obtained for blunt axisymmetric entry bodies...

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

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 description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies

Inouye, M.
Rakich, J. V.
Lomax, H.

August 1965

Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...

Application of a numerical orthogonal coordinate generator to axisymmetric blunt bodies /

Graves, Randolph A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 64."October 1979"--Cover."Langley Research Center."Includes bibliographical referen...

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

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...

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 /

Carson, George T.
Lee, Edwin E.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"December 1981"--Cover."Langley Research Center."Includes bibiliographical references.Mode of access...

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 method of integral relations solution for radiating, nonadiabatic, inviscid flow over a blunt body /

Suttles, John T. (John Timothy)
Langley Research Center.

Prepared at Langley Research Center."October 1969."Cover title.Includes bibliographical references (...

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...

Computation of equilibrium hypersonic flow about blunt axisymmetric bodies with sharp concers : (Final Report) /

Curtis, J. T., author.
Strom, C. R., author.
Sandia Corporation
U.S. Atomic Energy Commission.

"Purchase Orders 4804, Suborder 10 and 5003, Suborder 9.""August 1967."Includes bibliographical refe...

Calculation of axisymmetric laminar supersonic flow over blunt bodies

Mueller, B.
Oertel, H.
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V. (DFVLR), Goettingen (Germany). Aerodynamische Versuchsanstalt
Deutsche Forschungs- und Versuchsanstalt fuer Luft- und Raumfahrt e.V. (DFVLR), Goettingen (Germany). Inst. fuer Theoretische Stroemungsmechanik

January 1984

SIGLETIB: RN 9843 (84A02) / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische Informations...

Three-dimensional inviscid flow about supersonic blunt cones at angle of attack.

Moretti, G., author.
U.S. Atomic Energy Commission.
General Applied Science Laboratories (Westbury, Nassau County, N.Y.)
Sandia Corporation.

Comparisons are made between the cylindrical and polar coordinate system used in determining the thr...

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 ...

Viscous compressible flow about blunt bodies using a numerically generated orthogonal coordinate system

Hamilton, H. H., II
Graves, R. A., Jr.

July 1980

A numerical solution to the Navier-Stokes equations was obtained for blunt axisymmetric entry bodies...

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

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 description of numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over blunt-nosed and flared bodies

Inouye, M.
Rakich, J. V.
Lomax, H.

August 1965

Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...

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

Abstract

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

Abstract

Extracted data

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