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

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

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

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...

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...

The numerical calculation of laminar boundary-layer separation /

Klineberg, John M.
Steger, Joseph L.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 31-34).Mode of ...

An approximate method for calculating three-dimensional inviscid hypersonic flow fields /

Riley, Christopher J. (Christopher Joseph), 1964-
DeJarnette, Fred R.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

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...

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

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....

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Boundary-layer velocity profiles downstream of three-dimensional transition trips on a flat plate at Mach 3 and 4 /

Peterson, John B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at ...

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....

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...

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

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

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...

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...

The numerical calculation of laminar boundary-layer separation /

Klineberg, John M.
Steger, Joseph L.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 31-34).Mode of ...

An approximate method for calculating three-dimensional inviscid hypersonic flow fields /

Riley, Christopher J. (Christopher Joseph), 1964-
DeJarnette, Fred R.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

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...

Some simple solutions to the problem of predicting boundary-layer self-induced pressures /

Bertram, Michael H.
Blackstock, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

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....

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Boundary-layer velocity profiles downstream of three-dimensional transition trips on a flat plate at Mach 3 and 4 /

Peterson, John B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at ...

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....

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...

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

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

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

Abstract

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

Abstract

Extracted data

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