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

Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶ /

Hall, James R.
Piland, Robert O.
Speegle, Katherine C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"May 16, 1957."Includes bibliographical references (p. 11).Mode of access: Internet

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

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

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 ...

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...

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...

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....

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...

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...

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...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Flight measurement of wall-pressure fluctuations and boundary-layer turbulence /

Mull, Harold R.
Algranti, Joseph S.
Lewis Research Center.

January 1960

"NASA TN D-280.""Lewis Research Center, Cleveland, Ohio.""October 1960."Cover title.Includes bibliog...

Analysis of flight data on boundary layer transition at high angles of attack /

Haigh, Wayne W.
Ko, D. R. S.
Lake, B. M.
Langley Research Center.
TRW Systems Group.

January 1972

Boundary layer transition data were obtained on the flight of two cones which reentered at velocitie...

Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 /

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

Cover title."August 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid m...

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...

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 ...

Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶ /

Hall, James R.
Piland, Robert O.
Speegle, Katherine C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"May 16, 1957."Includes bibliographical references (p. 11).Mode of access: Internet

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

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

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 ...

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...

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...

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....

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...

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...

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...

Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 /

Rumsey, Charles B.
Lee, Dorothy B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics; Vehicle performan...

Flight measurement of wall-pressure fluctuations and boundary-layer turbulence /

Mull, Harold R.
Algranti, Joseph S.
Lewis Research Center.

January 1960

"NASA TN D-280.""Lewis Research Center, Cleveland, Ohio.""October 1960."Cover title.Includes bibliog...

Analysis of flight data on boundary layer transition at high angles of attack /

Haigh, Wayne W.
Ko, D. R. S.
Lake, B. M.
Langley Research Center.
TRW Systems Group.

January 1972

Boundary layer transition data were obtained on the flight of two cones which reentered at velocitie...

Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 /

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

Cover title."August 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid m...

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...

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 ...

Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶ /

Hall, James R.
Piland, Robert O.
Speegle, Katherine C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"May 16, 1957."Includes bibliographical references (p. 11).Mode of access: Internet

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

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

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 ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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