Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle /

Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers /

Ashby, George C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /

Stallings, Robert L.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"July 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

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...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 /

Penland, Jim A.
Hallissy, James B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"December 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 /

Riebe, Gregory D.
Pittman, Jimmy L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover."Langley Research Center."Mode of access: Internet

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...

Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers /

Ashby, George C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /

Stallings, Robert L.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"July 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

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...

Aerodynamic characteristics of three slender sharp-edge 74 ̊swept wings at subsonic, transonic, and supersonic Mach numbers /

Davenport, Edwin E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 /

Penland, Jim A.
Hallissy, James B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"December 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

Capone, Francis J.
Arbiter, Dorothy.
Bare, E. Ann.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 15-1...

Aerodynamic characteristics of a hypersonic cruise aircraft concept with wing-mounted propulsion systems at mach numbers of 2.96, 3.96, and 4.63 /

Riebe, Gregory D.
Pittman, Jimmy L.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover."Langley Research Center."Mode of access: Internet

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...

Longitudinal aerodynamic performance of a series of power-law and minimum-wave-drag bodies at Mach 6 and several Reynolds numbers /

Ashby, George C.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

Riebe, Gregory D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle /

Abstract

Extracted data

Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle /

Abstract

Extracted data

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