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

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall /

Muhlstein, Lado.
Beranek, Richard G.
George C. Marshall Space Flight Center.
Ames Research Center.

Prepared at Ames Research Center and Marshall Space Flight Center."August 1971."Cover title.Includes...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).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...

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...

Theoretical and experimental studies of reentry plasmas /

Dunn, M. G. (Michael G.)
Kang, Sang-Wook.
Langley Research Center.
Cornell Aeronautical Laboratory.

January 1973

"Prepared by Cornell Aeronautical Laboratory ... for Langley Research Center."Cover title.Bibliograp...

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

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....

An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube /

Weilmuenster, K. James.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Turbulent wall jet in a coflowing stream /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel /

Jones, Robert A.
Feller, William V.
Langley Research Center.

Prepared at Langley Research Center."February 1970."Cover title.Includes bibliographical references ...

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...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

On the theory of compliant wall drag reduction in turbulent boundary layers /

Ash, Robert L.
Langley Research Center.
Old Dominion University.

January 1974

"April 1974.""Prepared by Old Dominion University ... for Langley Research Center."Cover title.Inclu...

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall /

Muhlstein, Lado.
Beranek, Richard G.
George C. Marshall Space Flight Center.
Ames Research Center.

Prepared at Ames Research Center and Marshall Space Flight Center."August 1971."Cover title.Includes...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).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...

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...

Theoretical and experimental studies of reentry plasmas /

Dunn, M. G. (Michael G.)
Kang, Sang-Wook.
Langley Research Center.
Cornell Aeronautical Laboratory.

January 1973

"Prepared by Cornell Aeronautical Laboratory ... for Langley Research Center."Cover title.Bibliograp...

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

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....

An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube /

Weilmuenster, K. James.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Turbulent wall jet in a coflowing stream /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-19).Mode ...

Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel /

Jones, Robert A.
Feller, William V.
Langley Research Center.

Prepared at Langley Research Center."February 1970."Cover title.Includes bibliographical references ...

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...

Wind tunnel simulation of full scale vortices /

Rorke, James B.
Moffitt, Robert C.
Langley Research Center.
United Aircraft Corporation. Sikorsky Aircraft Division.

January 1973

"Prepared by Sikorsky Aircraft Division, United Aircraft Corporation ... for Langley Research Center...

On the theory of compliant wall drag reduction in turbulent boundary layers /

Ash, Robert L.
Langley Research Center.
Old Dominion University.

January 1974

"April 1974.""Prepared by Old Dominion University ... for Langley Research Center."Cover title.Inclu...

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 study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall /

Muhlstein, Lado.
Beranek, Richard G.
George C. Marshall Space Flight Center.
Ames Research Center.

Prepared at Ames Research Center and Marshall Space Flight Center."August 1971."Cover title.Includes...

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

Abstract

Extracted data

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

Abstract

Extracted data

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