Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case /

A viscous flow analysis for the tip vortex generation process /

Shamroth, S.J.
Briley, W. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

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

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual /

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

January 1981

STAR category 02."May 1981"--Cover.Includes bibliographical references.Mode of access: Internet

An implicit method for the calculation of inlet flow fields /

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

January 1981

"June 1981"--Cover."Nielsen Engineering & Research, Inc."Includes bibliographical references.Mode of...

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

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test case

Mcmillan, O. J.
Biringen, S.

June 1981

The source listing of a computer code for calculating the flow fields in a supersonic free stream is...

Calculation of two-dimensional inlet flow fields in a supersonic free strem by an implicit marching code with nonorthogonal mesh generation : user's manual /

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

January 1980

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

Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations /

Kumar, Ajay
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 07."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Analysis of the scramjet inlet flow field using two-dimensional Navier-Stokes equations /

Kumar, Ajay.
Tiwari, S. N.
Old Dominion University. Research Foundation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1982

"June 1982"--Cover."Old Dominion University Research Foundation"--Tech. rep. p.Includes bibliographi...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

An implicit numerical scheme for the simulation of internal viscous flows on unstructured grids /

Jorgenson, Philip C. E. (Philip Charles Eberhardt)
Pletcher, Richard H.
United States. National Aeronautics and Space Administration.

January 1994

Cover title.Includes bibliographical references (p. 15-16).Mode of access: Internet

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: User's manual

Mcmillan, O. J.
Biringen, S.

May 1981

Inlet flow fields for airbreathing missiles are calculated by the adaptation of a two dimensional co...

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

A viscous flow analysis for the tip vortex generation process /

Shamroth, S.J.
Briley, W. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

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

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects : User's manual /

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

January 1981

STAR category 02."May 1981"--Cover.Includes bibliographical references.Mode of access: Internet

An implicit method for the calculation of inlet flow fields /

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

January 1981

"June 1981"--Cover."Nielsen Engineering & Research, Inc."Includes bibliographical references.Mode of...

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

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test case

Mcmillan, O. J.
Biringen, S.

June 1981

The source listing of a computer code for calculating the flow fields in a supersonic free stream is...

Calculation of two-dimensional inlet flow fields in a supersonic free strem by an implicit marching code with nonorthogonal mesh generation : user's manual /

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

January 1980

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

Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations /

Kumar, Ajay
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 07."Langley Research Center.""December 1981"--Cover.Includes bibliographical refere...

Analysis of the scramjet inlet flow field using two-dimensional Navier-Stokes equations /

Kumar, Ajay.
Tiwari, S. N.
Old Dominion University. Research Foundation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1982

"June 1982"--Cover."Old Dominion University Research Foundation"--Tech. rep. p.Includes bibliographi...

Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies /

Reyhner, Theodore A.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

Subject Category 02."March 1982"--Cover.Includes bibliographical references.Mode of access: Internet

An implicit numerical scheme for the simulation of internal viscous flows on unstructured grids /

Jorgenson, Philip C. E. (Philip Charles Eberhardt)
Pletcher, Richard H.
United States. National Aeronautics and Space Administration.

January 1994

Cover title.Includes bibliographical references (p. 15-16).Mode of access: Internet

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: User's manual

Mcmillan, O. J.
Biringen, S.

May 1981

Inlet flow fields for airbreathing missiles are calculated by the adaptation of a two dimensional co...

Numerical calculations of two-dimensional, unsteady transonic flows with circulation /

Beam, Richard M.
Warming, Robert F. (Robert Fulton)
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 21-22).Mode of ...

Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /

Hawkins, J. E.
Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 46).Mode of access: Internet

A viscous flow analysis for the tip vortex generation process /

Shamroth, S.J.
Briley, W. R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

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

Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case /

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Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects - program documentation and test case /

Abstract

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