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

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 ...

Calculation of three-dimensional compressible laminar and turbulent boundary layers. Calculation of three-dimensional compressible boundary layers on arbitrary wings

Moser, A.
Kaups, K.
Cebeci, T.
Ramsey, J.

January 1975

A very general method for calculating compressible three-dimensional laminar and turbulent boundary ...

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....

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...

The calculation of three-dimensional turbulent boundary layers on helicopter rotors /

Hicks, J. G. (John G.)
Nash, J. F.
Lockheed-Georgia Company.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

"May 1971."Includes bibliographical references (p. 65)."Prepared under contract no.Mode of access: I...

Stability of three-dimensional compressible boundary layers /

Reshotko, Eli.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

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...

Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations /

Kuhn, Gary D.
United States. National Aeronautical and Space Administration.
Nielsen Engineering & Research.
Langley Research Center.

January 1971

"Prepared by Nielsen Engineering and Research, Inc. ... for Langley Research Center."N72-12222.Cover...

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....

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

Cebeci, T.
Kaups, K.
Ramsey, J. A.

January 1977

The method described utilizes a nonorthogonal coordinate system for boundary-layer calculations. It ...

The numerical computation of three-dimensional turbulent boundary layers

Smith, P.D.
Royal Aircraft Establishment, Farnborough (UK)

January 1982

SIGLELD:8670.2(RAE-TM-AERO--1945). / BLDSC - British Library Document Supply CentreGBUnited Kingdo

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 ...

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...

Calculation of laminar and turbulent boundary layers for two-dimensional time-dependent flows /

Cebeci, Tuncer.
California State University, Long Beach.
United States. National Aeronautics and Space Administration.

January 1977

Issued July 1977.Prepared by California State University at Long Beach under contract no. NAS 1-1365...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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 ...

Calculation of three-dimensional compressible laminar and turbulent boundary layers. Calculation of three-dimensional compressible boundary layers on arbitrary wings

Moser, A.
Kaups, K.
Cebeci, T.
Ramsey, J.

January 1975

A very general method for calculating compressible three-dimensional laminar and turbulent boundary ...

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....

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...

The calculation of three-dimensional turbulent boundary layers on helicopter rotors /

Hicks, J. G. (John G.)
Nash, J. F.
Lockheed-Georgia Company.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

"May 1971."Includes bibliographical references (p. 65)."Prepared under contract no.Mode of access: I...

Stability of three-dimensional compressible boundary layers /

Reshotko, Eli.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

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...

Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations /

Kuhn, Gary D.
United States. National Aeronautical and Space Administration.
Nielsen Engineering & Research.
Langley Research Center.

January 1971

"Prepared by Nielsen Engineering and Research, Inc. ... for Langley Research Center."N72-12222.Cover...

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....

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

Cebeci, T.
Kaups, K.
Ramsey, J. A.

January 1977

The method described utilizes a nonorthogonal coordinate system for boundary-layer calculations. It ...

The numerical computation of three-dimensional turbulent boundary layers

Smith, P.D.
Royal Aircraft Establishment, Farnborough (UK)

January 1982

SIGLELD:8670.2(RAE-TM-AERO--1945). / BLDSC - British Library Document Supply CentreGBUnited Kingdo

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 ...

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...

Calculation of laminar and turbulent boundary layers for two-dimensional time-dependent flows /

Cebeci, Tuncer.
California State University, Long Beach.
United States. National Aeronautics and Space Administration.

January 1977

Issued July 1977.Prepared by California State University at Long Beach under contract no. NAS 1-1365...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

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 ...

Calculation of three-dimensional compressible laminar and turbulent boundary layers. Calculation of three-dimensional compressible boundary layers on arbitrary wings

Moser, A.
Kaups, K.
Cebeci, T.
Ramsey, J.

January 1975

A very general method for calculating compressible three-dimensional laminar and turbulent boundary ...

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....

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

Abstract

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

Abstract

Extracted data

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