Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Pressures, forces and moments, and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in helium /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"January 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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...

Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic Mach-number flow /

Heller, H. (Hanno)
Clemente, Anthony R.
Langley Research Center.
Bolt, Beranek, and Newman, inc.

January 1974

"Prepared by Bolt, Beranek, and Newman ... for Langley Research Center."Cover title.Includes bibliog...

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-26).Mode ...

Pressure distributions on sphere cones /

Ellett, D. M.
Sandia Corporation.

January 1965

"Aerodynamics.""January 1965."Includes bibliographical references.Mode of access: Internet

Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances /

Sawyer, James Wayne.
Whitcomb, Charles F.
United States. National Aeronautics and Space Administration.

January 1971

N72-11009.Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and CO₂ flows, and calibration results in Langley 6-inch expansion tube /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 31-33).Mode ...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Theoretical prediction of pressures in hypersonic flow with special reference to configurations having attached leading-edge shock.

Scheuing, Richard A., author.
Melnik, Robert E., author.
Brook, John W., author.
Mead, Harold R., author.
Aeronautical Research Associates of Princeton. sponsor.
Grumman Aircraft Engineering Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body.
United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor.
United States. Aerospace Medical Division. sponsor.

"May 1962."Includes bibliographical references (pages 174-177).Flight Control Laboratory Contract No...

Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 /

Cubbison, Robert W.
Ward, James J.
Anderson, Bernhard H.
Lewis Research Center.

Prepared at Lewis Research Center."February 1961."Cover title.Includes bibliographical references (p...

Pressures, forces and moments, and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in helium /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"January 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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...

Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic Mach-number flow /

Heller, H. (Hanno)
Clemente, Anthony R.
Langley Research Center.
Bolt, Beranek, and Newman, inc.

January 1974

"Prepared by Bolt, Beranek, and Newman ... for Langley Research Center."Cover title.Includes bibliog...

Comparisons of theoretical and experimental pressure distributions over a wing-body model at high supersonic speeds /

Jernell, Lloyd S.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N71-35197.Cover title.Includes bibliographical references (p. 8)...

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

Fuller, Dennis E.
Langley Research Center.

January 1976

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 24-26).Mode ...

Pressure distributions on sphere cones /

Ellett, D. M.
Sandia Corporation.

January 1965

"Aerodynamics.""January 1965."Includes bibliographical references.Mode of access: Internet

Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances /

Sawyer, James Wayne.
Whitcomb, Charles F.
United States. National Aeronautics and Space Administration.

January 1971

N72-11009.Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air, and CO₂ flows, and calibration results in Langley 6-inch expansion tube /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 31-33).Mode ...

Pressure measurements on sharp and blunt 5 degreee and 15 degree-half-angle cones at mach number 3.86 and angles of attack to 100 degrees /

Amick, James L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibl...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Theoretical prediction of pressures in hypersonic flow with special reference to configurations having attached leading-edge shock.

Scheuing, Richard A., author.
Melnik, Robert E., author.
Brook, John W., author.
Mead, Harold R., author.
Aeronautical Research Associates of Princeton. sponsor.
Grumman Aircraft Engineering Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body.
United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor.
United States. Aerospace Medical Division. sponsor.

"May 1962."Includes bibliographical references (pages 174-177).Flight Control Laboratory Contract No...

Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 /

Cubbison, Robert W.
Ward, James J.
Anderson, Bernhard H.
Lewis Research Center.

Prepared at Lewis Research Center."February 1961."Cover title.Includes bibliographical references (p...

Pressures, forces and moments, and shock shapes for a geometrically matched sphere-cone and hyperboloid at Mach 20.3 in helium /

Calloway, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"January 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 /

Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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...

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Abstract

Extracted data

Measured pressure distributions on large-angle cones in hypersonic flows of tetrafluoromethane, air, and helium /

Abstract

Extracted data

Related items

Related items