Real-gas laminar boundary layers in hypervelocity nozzles /

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

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...

Real-gas effects in critical-flow-through nozzles and tabulated thermodynamic properties /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

Prepared at Lewis Research Center."January 1965"--Cover.Includes bibliographical references (p. 34-3...

Laminar boundary-layer separation induced by flares on cylinders with highly cooled boundary layers at a Mach number of 15 /

Kuehn, Donald M.
Ames Research Center.

Prepared at Ames Research Center."January 1965"--Cover.Includes bibliographical references (p. 9).Mo...

Boundary-layer transition under hypersonic conditions /

Potter, J. Leith. author.
Whitfield, Jack D., author.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.
ARO, Inc., sponsor.

"AGARDography 97, Part III.""Program Element 62405334, Project 8953, Task 895303.""May 1965."Include...

The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Project No. 1366.""May 1965."Includes bibliographical references (page 5)...

Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects /

Tolle, Ralph C., author.
Air Force Wright Aeronautical Laboratories. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.

"Final Report for 07/01/92--11/19/95.""October 1996."Includes bibliographical references (pages 161-...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

Flat-plate boundary-layer transition at hypersonic speeds /

Deem, R. E., author.
Murphy, J. S., author.
Erickson, C. R., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograpical references (pages 86-91).Print reproduction.Air Force Contrac...

The response of the laminar boundary layer to impulsive motions /

Rosenzweig, Martin Lewis, 1932-, author.
United States. Air Force. Office of Scientific Research, issuing body.
Cornell University, sponsor.

Research supported with funding from the United States Air Force, Mechanics Division of the Office o...

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 ...

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 ...

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...

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....

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

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...

Real-gas effects in critical-flow-through nozzles and tabulated thermodynamic properties /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

Prepared at Lewis Research Center."January 1965"--Cover.Includes bibliographical references (p. 34-3...

Laminar boundary-layer separation induced by flares on cylinders with highly cooled boundary layers at a Mach number of 15 /

Kuehn, Donald M.
Ames Research Center.

Prepared at Ames Research Center."January 1965"--Cover.Includes bibliographical references (p. 9).Mo...

Boundary-layer transition under hypersonic conditions /

Potter, J. Leith. author.
Whitfield, Jack D., author.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.
ARO, Inc., sponsor.

"AGARDography 97, Part III.""Program Element 62405334, Project 8953, Task 895303.""May 1965."Include...

The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Project No. 1366.""May 1965."Includes bibliographical references (page 5)...

Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects /

Tolle, Ralph C., author.
Air Force Wright Aeronautical Laboratories. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.

"Final Report for 07/01/92--11/19/95.""October 1996."Includes bibliographical references (pages 161-...

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...

Charts for equilibrium flow properties of air in hypervelocity nozzles /

Jorgensen, Leland H.
Baum, Geyle M.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

Flat-plate boundary-layer transition at hypersonic speeds /

Deem, R. E., author.
Murphy, J. S., author.
Erickson, C. R., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograpical references (pages 86-91).Print reproduction.Air Force Contrac...

The response of the laminar boundary layer to impulsive motions /

Rosenzweig, Martin Lewis, 1932-, author.
United States. Air Force. Office of Scientific Research, issuing body.
Cornell University, sponsor.

Research supported with funding from the United States Air Force, Mechanics Division of the Office o...

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 ...

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 ...

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...

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....

Charts for air flow properties in equilibrium and frozen flows in hypervelocity nozzles /

Yoshikawa, Kenneth K.
Katzen, Elliott D.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion syst...

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...

Real-gas effects in critical-flow-through nozzles and tabulated thermodynamic properties /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

Prepared at Lewis Research Center."January 1965"--Cover.Includes bibliographical references (p. 34-3...

Real-gas laminar boundary layers in hypervelocity nozzles /

Abstract

Extracted data

Real-gas laminar boundary layers in hypervelocity nozzles /

Abstract

Extracted data

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