Sphere-cone-cone surface pressure distribution at Mach numbers of 5, 6, 8, and 10 /

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

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

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure distributions on sphere cones /

Ellett, D. M.
Sandia Corporation.

January 1965

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

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

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

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Base pressure measurements on sharp and blunt 9©� cones at Mach numbers from 3.50 to 9.20 /

Zarin, Neil A. (Neil Arthur), 1938-
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT&E Project No. 1A222901A201.""November 1965."Includes bibliographical references (page 35).Mode ...

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...

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

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).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

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

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

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure distributions on sphere cones /

Ellett, D. M.
Sandia Corporation.

January 1965

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

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

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

Comparison of experimental and theoretical shock shapes and pressure distributions on flat-faced cylinders at Mach 10.5 /

Inouye, Mamoru.
Sinclair, A. Richard.
Marvin, Joseph G.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."February 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Zarin, Neil A. (Neil Arthur), 1938-
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT&E Project No. 1A222901A201.""November 1965."Includes bibliographical references (page 35).Mode ...

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...

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

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Supersonic aerodynamics of large-angle cones /

Campbell, James F.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."August 1968."Includes bibliographical references (p. 13).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

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

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

Jones, Robert A.
Hunt, James L. (James Larry), 1939-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle /

Blackwell, James A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

Cover title."March 1966."Includes bibliographical references (p. 7).Mode of access: Internet

Sphere-cone-cone surface pressure distribution at Mach numbers of 5, 6, 8, and 10 /

Abstract

Extracted data

Sphere-cone-cone surface pressure distribution at Mach numbers of 5, 6, 8, and 10 /

Abstract

Extracted data

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