Boundary-layer transition under hypersonic conditions /

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...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

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...

Theoretical and experimental studies of hypersonic viscous effects /

Lewis, Clark H. (Clark Houston), 1929-. 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...

Boundary layer transition and surface roughness effects in hypersonic flow /

Holden, Michael S., author.
Calspan Corporation. Advanced Technology Center. sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Calspan Report No. 6430-A-1.""Calspan Advanced Technology Center, Buffalo, New York.""Annual Report...

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...

Investigation of supersonic boundary layer transition and turbulent structure /

Smits, Alexander J., author.
Miles, R. B., author.
Princeton University. Gas Dynamics Laboratory. sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Final Technical Report from December 1, 1988 to March 1, 1990.""July 15, 1990."Includes bibliograph...

Two techniques for detecting boundary-layer transition in flight at supersonic speeds and at altitudes above 20,000 feet /

McTigue, John G.
Petty, Gilbert.
Overton, John D.
Flight Research Center (U.S.)

January 1959

"NASA TN D-18.""High-Speed Flight Station, Edwards, Calif.""August 1959."Cover title.Includes biblio...

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 boundary-layer transition on a 10 ̊half-angle cone at Mach 6.9 /

Fischer, Michael C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Boundary layer transition on nose cones at hypersonic speeds.Includes bibliographical references (p....

Real-gas laminar boundary layers in hypervelocity nozzles /

Summers, Willard E., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62410034, Task 777805.""October 1965."Includes bibliographical references (pages 21...

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 ...

Investigation of boundary-layer transition on swept wings at mach numbers 2.5 to 5 /

Pate, S. R., author.
Brillhart, R. E., author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted by the von Kármán Gas Dynamics Facility, ARO, In.""ARO Project No. VD0318.""AFSC...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

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...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

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...

Theoretical and experimental studies of hypersonic viscous effects /

Lewis, Clark H. (Clark Houston), 1929-. 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...

Boundary layer transition and surface roughness effects in hypersonic flow /

Holden, Michael S., author.
Calspan Corporation. Advanced Technology Center. sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Calspan Report No. 6430-A-1.""Calspan Advanced Technology Center, Buffalo, New York.""Annual Report...

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...

Investigation of supersonic boundary layer transition and turbulent structure /

Smits, Alexander J., author.
Miles, R. B., author.
Princeton University. Gas Dynamics Laboratory. sponsor.
United States. Air Force. Office of Scientific Research. issuing body.

"Final Technical Report from December 1, 1988 to March 1, 1990.""July 15, 1990."Includes bibliograph...

Two techniques for detecting boundary-layer transition in flight at supersonic speeds and at altitudes above 20,000 feet /

McTigue, John G.
Petty, Gilbert.
Overton, John D.
Flight Research Center (U.S.)

January 1959

"NASA TN D-18.""High-Speed Flight Station, Edwards, Calif.""August 1959."Cover title.Includes biblio...

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 boundary-layer transition on a 10 ̊half-angle cone at Mach 6.9 /

Fischer, Michael C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Boundary layer transition on nose cones at hypersonic speeds.Includes bibliographical references (p....

Real-gas laminar boundary layers in hypervelocity nozzles /

Summers, Willard E., author.
ARO, Inc. sponsor.
United States. Air Force. Arnold Air Force Base. sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62410034, Task 777805.""October 1965."Includes bibliographical references (pages 21...

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 ...

Investigation of boundary-layer transition on swept wings at mach numbers 2.5 to 5 /

Pate, S. R., author.
Brillhart, R. E., author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted by the von Kármán Gas Dynamics Facility, ARO, In.""ARO Project No. VD0318.""AFSC...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

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...

Some effects of leading-edge sweep on boundary-layer transition at supersonic speeds /

Chapman, Gary T.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Flui...

Effects of mach number, leading edge bluntness and sweep on boundary-layer transition on a flat plate /

Jillie, Don W.
Hopkins, Edward J.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bib...

Boundary-layer transition under hypersonic conditions /

Abstract

Extracted data

Boundary-layer transition under hypersonic conditions /

Abstract

Extracted data

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