An experimental investigation of turbulent boundary layers along curved surfaces /

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...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures /

Corke, T. C.
Nagib, Hassan M.
Guezennec, Y.
Illinois Institute of Technology.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."Illinois Institute of Technology."Includes bibliographical references.Mode of ac...

Experimental data and model for the turbulent boundary layer on a convex, curved surface /

Gillis, J. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 34."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

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....

Turbulent boundary layer heat transfer experiments : convex curvature effects including introduction and recovery /

Simon, T. W.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1982

"February 1982"--Cover.Subject category 34.Includes bibliographical references.Mode of access: Inter...

An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. /

Gault, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Natural laminar flow experiments on modern airplane surfaces /

Holmes, Bruce J.
Yip, Long P.
Obara, Clifford J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."June 1984"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Experimental investigation of laminar-flow separation on a flat plate induced by deflected trailing-edge flap at Mach 19 /

Harvey, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 22-25).Mode of access: Internet

Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing /

Czarnecki, K. R.
Sevier, John R.
United States. National Aeronautics and Space Administration.

Cover title."June 1960."Flow, laminar; Flow, turbulent; Aerodynamics with heat; Surface conditions,...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of the mixing and combustion of turbulent, compressible free jets /

Cohen, Leonard S.
Guile, Roy N.
United Aircraft Corporation. Research Laboratories.

"December 1969"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures /

Corke, T. C.
Nagib, Hassan M.
Guezennec, Y.
Illinois Institute of Technology.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."Illinois Institute of Technology."Includes bibliographical references.Mode of ac...

Experimental data and model for the turbulent boundary layer on a convex, curved surface /

Gillis, J. C.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 34."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

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...

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....

Turbulent boundary layer heat transfer experiments : convex curvature effects including introduction and recovery /

Simon, T. W.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1982

"February 1982"--Cover.Subject category 34.Includes bibliographical references.Mode of access: Inter...

An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. /

Gault, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Natural laminar flow experiments on modern airplane surfaces /

Holmes, Bruce J.
Yip, Long P.
Obara, Clifford J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."June 1984"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Experimental investigation of laminar-flow separation on a flat plate induced by deflected trailing-edge flap at Mach 19 /

Harvey, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 22-25).Mode of access: Internet

Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing /

Czarnecki, K. R.
Sevier, John R.
United States. National Aeronautics and Space Administration.

Cover title."June 1960."Flow, laminar; Flow, turbulent; Aerodynamics with heat; Surface conditions,...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of the mixing and combustion of turbulent, compressible free jets /

Cohen, Leonard S.
Guile, Roy N.
United Aircraft Corporation. Research Laboratories.

"December 1969"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures /

Corke, T. C.
Nagib, Hassan M.
Guezennec, Y.
Illinois Institute of Technology.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."Illinois Institute of Technology."Includes bibliographical references.Mode of ac...

An experimental investigation of turbulent boundary layers along curved surfaces /

Abstract

Extracted data

An experimental investigation of turbulent boundary layers along curved surfaces /

Abstract

Extracted data

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