Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 /

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Pressure distributions induced by elevon deflections on swept wings and adjacent end-plate surfaces at Mach 6 /

Kaufman, Louis G., II.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Prepared by Langley Research Center, Hampton, VA 23665.Includes bibliographical references (p. 13-1...

Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 /

Deveikis, William D.
Bartlett, Whitney.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Dec. 1978."Langley Research Center, Hampton, Virginia."Includes bibliographical references.Mode of a...

Heat-transfer measurements in free flight at Mach numbers up to 14.6 on a flat-faced conical nose with a total angle of 29©� /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"January 24, 1958; Declassified February 8, 1963."Includes bibliographical references (p. 17).Mode o...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls.

Kaufman, Louis G., II., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Grumman Aircraft Engineering Corporation. Research Department. sponsor.

Includes bibliograpical references (pages 7-8 ).Air Force Contract No.Mode of access: Internet

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Measurements of aerodynamic heat transfer in turbulent separated regions at a Mach number of 1.8 /

Garland, Benjamine J.
Hall, James R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 20, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

Jones, Ira P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Pressure distributions induced by elevon deflections on swept wings and adjacent end-plate surfaces at Mach 6 /

Kaufman, Louis G., II.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Prepared by Langley Research Center, Hampton, VA 23665.Includes bibliographical references (p. 13-1...

Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 /

Deveikis, William D.
Bartlett, Whitney.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Dec. 1978."Langley Research Center, Hampton, Virginia."Includes bibliographical references.Mode of a...

Heat-transfer measurements in free flight at Mach numbers up to 14.6 on a flat-faced conical nose with a total angle of 29©� /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"January 24, 1958; Declassified February 8, 1963."Includes bibliographical references (p. 17).Mode o...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls.

Kaufman, Louis G., II., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Grumman Aircraft Engineering Corporation. Research Department. sponsor.

Includes bibliograpical references (pages 7-8 ).Air Force Contract No.Mode of access: Internet

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71 /

Morris, W. Douglas.
Couch, Lana M.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 12).Mode of access: Internet

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Measurements of aerodynamic heat transfer in turbulent separated regions at a Mach number of 1.8 /

Garland, Benjamine J.
Hall, James R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 20, 1958."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

Jones, Ira P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 /

Rumsey, Charles B.
Lee, Dorothy B.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 /

Abstract

Extracted data

Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 /

Abstract

Extracted data

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