Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 /

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

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

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

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...

Aerothermal analysis of a wing-elevon cove with variable leakage /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Includes bibliographical references.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...

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...

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

Bartlett, W.
Deveikis, W. D.

December 1978

An experimental aerodynamic heating investigation was conducted to determine effects of hot boundary...

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

Johnson, Charles B.
Weinstein, Irving, joint author.
Taylor, Allan H., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 12).Mode of access: Internet

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction /

Brown, Ronald D.
Jakubowski, Antoni K. (Antoni Karol), 1920-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Effect of two-dimensional multiple sine-wave protrusions on the pressure and heat-transfer distributions for a flat plate at Mach 6 /

Cary, Aubrey M.
Morrisette, E. Leon.
Langley Research Center.

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 22-2...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

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

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

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...

Aerothermal analysis of a wing-elevon cove with variable leakage /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Includes bibliographical references.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...

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...

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

Bartlett, W.
Deveikis, W. D.

December 1978

An experimental aerodynamic heating investigation was conducted to determine effects of hot boundary...

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

Johnson, Charles B.
Weinstein, Irving, joint author.
Taylor, Allan H., joint author.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 12).Mode of access: Internet

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction /

Brown, Ronald D.
Jakubowski, Antoni K. (Antoni Karol), 1920-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Effect of two-dimensional multiple sine-wave protrusions on the pressure and heat-transfer distributions for a flat plate at Mach 6 /

Cary, Aubrey M.
Morrisette, E. Leon.
Langley Research Center.

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 22-2...

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

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

Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium /

Marvin, Joseph G.
Ames Research Center.

January 1963

"April 1963."Cover title.Includes bibliographical references (p. 13-14).Mode of access: Internet

Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 /

Abstract

Extracted data

Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 /

Abstract

Extracted data

Related items

Related items