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

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

A study of boundary layer transition on outgassing cones in hypersonic flow /

Stalmach, C. J.
United States. National Aeronautics and Space Administration.
Vought Aeronautics Company.
Langley Research Center.

January 1971

Prepared by Vought Aeronautics Company for Langley Research Center.N72-12225.Includes bibliographica...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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 ...

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 ...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Murthy, A. V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

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...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

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 ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

A study of boundary layer transition on outgassing cones in hypersonic flow /

Stalmach, C. J.
United States. National Aeronautics and Space Administration.
Vought Aeronautics Company.
Langley Research Center.

January 1971

Prepared by Vought Aeronautics Company for Langley Research Center.N72-12225.Includes bibliographica...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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 ...

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 ...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Murthy, A. V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

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...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

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 ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

Prepared at Langley Research Center."September 1985"--Cover.Includes bibliographical references (p. ...

Weak incident shock interactions with Mach 8 laminar boundary layers /

Kaufman, Louis G.
Johnson, Charles B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21-23).Mode ...

Flight-measured laminar boundary layer transition phenomena including stability theory analysis /

Obara, Clifford J.
Holmes, Bruce J.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 8).M...

Pressure distributions and shock shapes for 12.84/̊7 ̊on-axis and bent-nose biconics in air at mach 6 /

Miller, Charles G. (Charles George), 1940-
Gnoffo, Peter A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."December 1981"--Cover."Langley Research Center."Mode of access: Internet

A study of boundary layer transition on outgassing cones in hypersonic flow /

Stalmach, C. J.
United States. National Aeronautics and Space Administration.
Vought Aeronautics Company.
Langley Research Center.

January 1971

Prepared by Vought Aeronautics Company for Langley Research Center.N72-12225.Includes bibliographica...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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

Abstract

Extracted data

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

Abstract

Extracted data

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