Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.

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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Pressure measurements for Mach five flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics /

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

"January 1964."Includes bibliographical references (page 5).Air Force Contract No.Mode of access: In...

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

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 ...

Pressure data for four analytically defined arrow wings in supersonic flow /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Bibliography: p. 16.Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Unsteady aerodynamics for advanced configurations.

Li, T. C., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

Includes bibliograpical references (page 42).Air Force Contract No.Mode of access: Internet

Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /

Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"April 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

Nugent, Jack.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Pressure measurements for Mach five flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics /

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

"January 1964."Includes bibliographical references (page 5).Air Force Contract No.Mode of access: In...

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

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 ...

Pressure data for four analytically defined arrow wings in supersonic flow /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Sept. 1980."Langley Research Center."Bibliography: p. 16.Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Unsteady aerodynamics for advanced configurations.

Li, T. C., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

Includes bibliograpical references (page 42).Air Force Contract No.Mode of access: Internet

Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /

Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"April 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

Nugent, Jack.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).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

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.

Abstract

Extracted data

Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.

Abstract

Extracted data

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