Three-dimensional compressible turbulent computations for a diffusing S-duct /

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 ...

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...

Three-dimensional turbulent boundary layers /

Sendstad, O., author.
Moin, Parviz. author.
Stanford University. Stanford University. Thermosciences Division sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Prepared with support of the Air Force Office of Scientific Research under Grants 87-0285 and 91-01...

Three-dimensional compressible turbulent computations for a nondiffusing S-duct /

Harloff, G. J. (Gary James), 1945-
Lewis Research Center.
Sverdrup Technology, Inc.

January 1992

Prepared at Sverdrup Technology, Inc., for Lewis Research Center under Contract NAS3-25266.Includes ...

A Three-dimensional turbulent compressible subsonic duct flow analysis for use with constructed coordinate systems /

Levy, R. (Ralph), 1945-
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Apr. 1981."Prepared for Lewis Research Center under contract NAS3-21735."Includes bibliographical re...

Development of a three-dimensional turbulent duct flow analysis /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Eiseman, P. R.
Lewis Research Center.
United Technologies Research Center.

January 1978

Nov. 1978.Contract NAS3-19856.Includes bibliographical references.Mode of access: Internet

Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts /

Anderson, O. L. (Olos Lennart), 1931-
Lewis Research Center.
United Aircraft Corporation.

January 1974

"Prepared by United Aircraft Corporation ... for Lewis Research Center."Cover title.Bibliography: p....

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...

Computational study of compressible flow in an S-shaped duct

Suratanakavikul, V.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN034576 / BLDSC - British Library D...

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

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

January 1972

"Prepared by General Applied Science Laboratories, Inc., Westbury, New York ... for Langley Research...

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....

Numerical Investigation of 3D Compressible Duct Flow with Shock-Wave/Turbulent Boundary-Layer Interaction

Martina Blom
Martina I. M. Blom

January 2010

publish the Work electronically and in a non-commercial purpose make it accessible on the Internet. ...

WIND : computer program for calculation of three-dimensional potential compressible flow about wind turbine rotor blades /

Dulikravich, Djordje S.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow /

Albers, James A.
Gregg, John L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 168-169).Mode ...

Calculations of turbulent separated flows /

Zhu, J.
Shih, T. H.
United States. National Aeronautics and Space Administration.

January 1993

["August 1993."].NASA TM-106154.Includes bibliographical references (p. 10-12).Mode of access: Inter...

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 ...

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...

Three-dimensional turbulent boundary layers /

Sendstad, O., author.
Moin, Parviz. author.
Stanford University. Stanford University. Thermosciences Division sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Prepared with support of the Air Force Office of Scientific Research under Grants 87-0285 and 91-01...

Three-dimensional compressible turbulent computations for a nondiffusing S-duct /

Harloff, G. J. (Gary James), 1945-
Lewis Research Center.
Sverdrup Technology, Inc.

January 1992

Prepared at Sverdrup Technology, Inc., for Lewis Research Center under Contract NAS3-25266.Includes ...

A Three-dimensional turbulent compressible subsonic duct flow analysis for use with constructed coordinate systems /

Levy, R. (Ralph), 1945-
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Apr. 1981."Prepared for Lewis Research Center under contract NAS3-21735."Includes bibliographical re...

Development of a three-dimensional turbulent duct flow analysis /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Eiseman, P. R.
Lewis Research Center.
United Technologies Research Center.

January 1978

Nov. 1978.Contract NAS3-19856.Includes bibliographical references.Mode of access: Internet

Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts /

Anderson, O. L. (Olos Lennart), 1931-
Lewis Research Center.
United Aircraft Corporation.

January 1974

"Prepared by United Aircraft Corporation ... for Lewis Research Center."Cover title.Bibliography: p....

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...

Computational study of compressible flow in an S-shaped duct

Suratanakavikul, V.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN034576 / BLDSC - British Library D...

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

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

January 1972

"Prepared by General Applied Science Laboratories, Inc., Westbury, New York ... for Langley Research...

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....

Numerical Investigation of 3D Compressible Duct Flow with Shock-Wave/Turbulent Boundary-Layer Interaction

Martina Blom
Martina I. M. Blom

January 2010

publish the Work electronically and in a non-commercial purpose make it accessible on the Internet. ...

WIND : computer program for calculation of three-dimensional potential compressible flow about wind turbine rotor blades /

Dulikravich, Djordje S.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow /

Albers, James A.
Gregg, John L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 168-169).Mode ...

Calculations of turbulent separated flows /

Zhu, J.
Shih, T. H.
United States. National Aeronautics and Space Administration.

January 1993

["August 1993."].NASA TM-106154.Includes bibliographical references (p. 10-12).Mode of access: Inter...

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 ...

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...

Three-dimensional turbulent boundary layers /

Sendstad, O., author.
Moin, Parviz. author.
Stanford University. Stanford University. Thermosciences Division sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Prepared with support of the Air Force Office of Scientific Research under Grants 87-0285 and 91-01...

Three-dimensional compressible turbulent computations for a diffusing S-duct /

Abstract

Extracted data

Three-dimensional compressible turbulent computations for a diffusing S-duct /

Abstract

Extracted data

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