An implicit method for the calculation of inlet flow fields /

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...

Equations for the rapid machine computation of equilibrium composition of air and derivatives for flow-field calculations /

Smith, G. Louis.
Eastwood, Mary R.
Erickson, Wayne D. (Wayne Douglas), 1932-
United States. National Aeronautics and Space Administration.

January 1967

Cover title."October 1967."Includes bibliographical references (p. 39).Mode of access: Internet

Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics /

Schweikhard, William G.
Chen, Yen-Sen.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."February 1983"--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 /

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

January 1981

Chiefly tables."June 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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

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

A simple computer model for evaluating coastal inlet hydraulics /

Seelig, William N.
Coastal Engineering Research Center (U.S.)

"July 1977."Cover title.Includes bibliographical references.Mode of access: Internet

DYNLET1 : dynamic implicit numerical model of one-dimensional tidal flow through inlets /

Amein, Michael, 1926-
Kraus, Nicholas C.
U.S. Army Engineer Waterways Experiment Station.
United States. Army. Corps of Engineers.

Cover title."September 1991."Includes bibliographical references (p. 76-79).Final report.Inlet Stabi...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis 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

The flow of water in flumes /

Scobey, Fred C. (Frederick Charles), 1880-1962.

January 1933

Contribution from Bureau of Agricultural Engineering.Cover title.Includes bibliographical references...

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

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

Calibration and testing of selected portable flowmeters for use on large irrigation systems /

Luckey, Richard R.
Gaggiani, Neville G.
Heimes, Frederick J.
Geological Survey (U.S.). Water Resources Division.

January 1980

"September 1980."--P. 2 of cover.Includes bibliographical references (p. 21).Mode of access: Interne...

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...

FORTRAN program to generate engine inlet flow contour maps and distortion parameters /

Dicus, John H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ac...

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...

Equations for the rapid machine computation of equilibrium composition of air and derivatives for flow-field calculations /

Smith, G. Louis.
Eastwood, Mary R.
Erickson, Wayne D. (Wayne Douglas), 1932-
United States. National Aeronautics and Space Administration.

January 1967

Cover title."October 1967."Includes bibliographical references (p. 39).Mode of access: Internet

Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics /

Schweikhard, William G.
Chen, Yen-Sen.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."February 1983"--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 /

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

January 1981

Chiefly tables."June 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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

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

A simple computer model for evaluating coastal inlet hydraulics /

Seelig, William N.
Coastal Engineering Research Center (U.S.)

"July 1977."Cover title.Includes bibliographical references.Mode of access: Internet

DYNLET1 : dynamic implicit numerical model of one-dimensional tidal flow through inlets /

Amein, Michael, 1926-
Kraus, Nicholas C.
U.S. Army Engineer Waterways Experiment Station.
United States. Army. Corps of Engineers.

Cover title."September 1991."Includes bibliographical references (p. 76-79).Final report.Inlet Stabi...

Development of a three-dimensional supersonic inlet flow analysis /

Buggeln, R. C.
Lewis 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

The flow of water in flumes /

Scobey, Fred C. (Frederick Charles), 1880-1962.

January 1933

Contribution from Bureau of Agricultural Engineering.Cover title.Includes bibliographical references...

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

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

Calibration and testing of selected portable flowmeters for use on large irrigation systems /

Luckey, Richard R.
Gaggiani, Neville G.
Heimes, Frederick J.
Geological Survey (U.S.). Water Resources Division.

January 1980

"September 1980."--P. 2 of cover.Includes bibliographical references (p. 21).Mode of access: Interne...

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...

FORTRAN program to generate engine inlet flow contour maps and distortion parameters /

Dicus, John H.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ac...

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...

Equations for the rapid machine computation of equilibrium composition of air and derivatives for flow-field calculations /

Smith, G. Louis.
Eastwood, Mary R.
Erickson, Wayne D. (Wayne Douglas), 1932-
United States. National Aeronautics and Space Administration.

January 1967

Cover title."October 1967."Includes bibliographical references (p. 39).Mode of access: Internet

Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics /

Schweikhard, William G.
Chen, Yen-Sen.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."February 1983"--Cover.Includes bibliographical references.Mode of access: Internet

An implicit method for the calculation of inlet flow fields /

Abstract

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An implicit method for the calculation of inlet flow fields /

Abstract

Extracted data

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