Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

Digital enhancement of flow field images /

Kudlinski, Robert A.
Park, Stephen Keith.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 6).M...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel /

Jones, Robert A.
Feller, William V.
Langley Research Center.

Prepared at Langley Research Center."February 1970."Cover title.Includes bibliographical references ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps /

Yip, Long P.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 7).Mod...

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Theoretical and experimental flow fields for a supersonic cruise fighter forebody /

Yaros, Steven F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 7...

Digital enhancement of flow field images /

Kudlinski, Robert A.
Park, Stephen Keith.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 6).M...

Semianalytic modeling of aerodynamic shapes /

Barger, Raymond L.
Adams, Mary S.
Langley Research Center.

January 1985

Prepared at Langley Research Center."April 1985"--Cover.Includes bibliographical references (p. 6).M...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel /

Jones, Robert A.
Feller, William V.
Langley Research Center.

Prepared at Langley Research Center."February 1970."Cover title.Includes bibliographical references ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps /

Yip, Long P.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 7).Mod...

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86 /

Stallings, Robert L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1981

"February 1984"--Cover.Includes bibliographical references.Mode of access: Internet

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Abstract

Extracted data

Mach 6 flow field surveys beneath the forebody of an airbreatinng missile /

Abstract

Extracted data

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