Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 /

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...

Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

Kussoy, Marvin.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins /

Cubbage, James M.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Propulsion system elements.Inc...

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...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

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 distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

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

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...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

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 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 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

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)...

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

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...

Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

Kussoy, Marvin.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins /

Cubbage, James M.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Propulsion system elements.Inc...

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...

Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Shrout, Barrett L.
Collins, Ida K.
Corlett, William A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Subject category 02."May 1979"--Cover."Langley Research Center."Includes bibliographical references....

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 distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

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

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...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

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 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 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

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)...

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

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...

Local pressure distribution on a blunt delta wing for angles of attack up to 35 degrees at Mach numbers of 3.4 and 4.7

Kussoy, Marvin.
United States. National Aeronautics and Space Administration.

Cover title."December 1962."Includes bibliographical references.Mode of access: Internet

Measured base pressures on several twin rocket-nozzle configurations at mach nubmers of 0.6 to 1.4 with effects due to nozzle canting and stabilizing fins /

Cubbage, James M.
Andrews, Earl H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, missiles and space vehicles; Propulsion system elements.Inc...

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 /

Abstract

Extracted data

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 /

Abstract

Extracted data

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