Analysis of variable property turbulent boundary layers by means of a modified compressibility transformation /

Contribution to the calculation of turbulent boundary layers.

Rotta, Julius C., 1912-

January 1951

"Report issued by the Max-Planck-Institut für Strömungsforschung in Göttingen; July 1, 1950."Bibl...

Wave theory of turbulence in compressible media /

Kentzer, Czeslaw P.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Purdue University.

January 1976

Cover title.Includes bibliographical references (p. 109-112).Mode of access: Internet

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

Parametric study of relaminarization of turbulent boundary layers on nozzle walls /

Kreskovsky, J. P.
McDonald, H. (Henry), 1937-
Shamroth, S. J.
Langley Research Center.
United Aircraft Corporation. Research Laboratories.

January 1974

"Prepared by United Aircraft Research Laboratories ... for Langley Research Center."Cover title.Bibl...

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

Computer program for calculating laminar and turbulent boundary layer development in compressible flow /

Herring, H. J.
Mellor, G. L.
Lewis Research Center.
Princeton University.

January 1972

"Prepared by Princeton University ... for Lewis Research Center."Cover title.Bibliography: p. 86-87....

The compressible turbulent boundary layer with surface mass transfer /

Culick, F. (Fred), 1933-, author.
United States. Air Force. Office of Scientific Research, issuing body.
Massachusetts Institute of Technology. Naval Supersonic Laboratory, sponsor.

Research supported with funding from the United States Air Force Office of Scientific Research, Air ...

Analysis of unsteady thermal boundary layers /

Miller, Roy W.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 80-81.Mode of access: Internet

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) /

Schmidt, James F.
Todd, Carroll A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22-23).Mode of...

A boundary layer approach to the analysis of atmospheric motion over a surface obstruction /

Frost, Walter, 1935-
Simpson, W. R.
Maus, J. R.
George C. Marshall Space Flight Center.
University of Tennessee (System). Space Institute.

January 1973

"Prepared by the University of Tennessee Space Institute ... for George C. Marshall Space Flight Cen...

On the wall-normal velocity of the compressible boundary-layer equations /

Pruett, C. David (Charles David), 1948-
Analytical Services and Materials, Inc.
Langley Research Center.

January 1991

Prepared at Analytical Services and Materials, Inc., for Langley Research Center under Contract NAS1...

Some problems of the calculation of three-dimensional boundary-layer flows on general configurations /

Cebeci, Tuncer.
Langley Research Center.
Douglas Aircraft Company.

January 1973

"Prepared by Douglas Aircraft Company, McDonnell Douglas Corporation ... for Langley Research Center...

An investigation of the high speed turbulent boundary layer with heat transfer and arbitrary pressure gradient /

Economos, Constantino.
Boccio, J. L.
Langley Research Center.
General Applied Science Laboratories (Westbury, Nassau County, N.Y.)

January 1970

This report investigates the behavior of high speed turbulent boundary layer with heat transfer and ...

Contribution to the calculation of turbulent boundary layers.

Rotta, Julius C., 1912-

January 1951

"Report issued by the Max-Planck-Institut für Strömungsforschung in Göttingen; July 1, 1950."Bibl...

Wave theory of turbulence in compressible media /

Kentzer, Czeslaw P.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Purdue University.

January 1976

Cover title.Includes bibliographical references (p. 109-112).Mode of access: Internet

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

Parametric study of relaminarization of turbulent boundary layers on nozzle walls /

Kreskovsky, J. P.
McDonald, H. (Henry), 1937-
Shamroth, S. J.
Langley Research Center.
United Aircraft Corporation. Research Laboratories.

January 1974

"Prepared by United Aircraft Research Laboratories ... for Langley Research Center."Cover title.Bibl...

An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient /

Zakkay, Victor.
Calarese, Wladimiro.
Langley Research Center.
New York University.

January 1972

"Prepared by New York University ... for Langley Research Center."Cover title.Bibliography: p. 9.Mod...

The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing /

Hunt, James L. (James Larry), 1939-
Beckwith, Ivan E.
Bushnell, Dennis M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."March 1971."Cover title.Includes bibliographical references (p....

Computer program for calculating laminar and turbulent boundary layer development in compressible flow /

Herring, H. J.
Mellor, G. L.
Lewis Research Center.
Princeton University.

January 1972

"Prepared by Princeton University ... for Lewis Research Center."Cover title.Bibliography: p. 86-87....

The compressible turbulent boundary layer with surface mass transfer /

Culick, F. (Fred), 1933-, author.
United States. Air Force. Office of Scientific Research, issuing body.
Massachusetts Institute of Technology. Naval Supersonic Laboratory, sponsor.

Research supported with funding from the United States Air Force Office of Scientific Research, Air ...

Analysis of unsteady thermal boundary layers /

Miller, Roy W.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 80-81.Mode of access: Internet

A general method for calculating three-dimensional compressible laminar and turbulent boundary layers on arbitrary wings /

Cebeci, Tuncer.
Ramsey, Judy A., joint author.
Kaups, Kalle, joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1977

Issued Jan. 1977.Prepared by McDonnell Douglas Corporation for Langley Research Center under NAS1-12...

Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) /

Schmidt, James F.
Todd, Carroll A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22-23).Mode of...

A boundary layer approach to the analysis of atmospheric motion over a surface obstruction /

Frost, Walter, 1935-
Simpson, W. R.
Maus, J. R.
George C. Marshall Space Flight Center.
University of Tennessee (System). Space Institute.

January 1973

"Prepared by the University of Tennessee Space Institute ... for George C. Marshall Space Flight Cen...

On the wall-normal velocity of the compressible boundary-layer equations /

Pruett, C. David (Charles David), 1948-
Analytical Services and Materials, Inc.
Langley Research Center.

January 1991

Prepared at Analytical Services and Materials, Inc., for Langley Research Center under Contract NAS1...

Some problems of the calculation of three-dimensional boundary-layer flows on general configurations /

Cebeci, Tuncer.
Langley Research Center.
Douglas Aircraft Company.

January 1973

"Prepared by Douglas Aircraft Company, McDonnell Douglas Corporation ... for Langley Research Center...

An investigation of the high speed turbulent boundary layer with heat transfer and arbitrary pressure gradient /

Economos, Constantino.
Boccio, J. L.
Langley Research Center.
General Applied Science Laboratories (Westbury, Nassau County, N.Y.)

January 1970

This report investigates the behavior of high speed turbulent boundary layer with heat transfer and ...

Contribution to the calculation of turbulent boundary layers.

Rotta, Julius C., 1912-

January 1951

"Report issued by the Max-Planck-Institut für Strömungsforschung in Göttingen; July 1, 1950."Bibl...

Wave theory of turbulence in compressible media /

Kentzer, Czeslaw P.
United States. National Aeronautics and Space Administration.
Langley Research Center.
Purdue University.

January 1976

Cover title.Includes bibliographical references (p. 109-112).Mode of access: Internet

An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /

Gupta, Roop N.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 73-75).Mode ...

Analysis of variable property turbulent boundary layers by means of a modified compressibility transformation /

Abstract

Extracted data

Analysis of variable property turbulent boundary layers by means of a modified compressibility transformation /

Abstract

Extracted data

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