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

Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model /

Hoad, Danny R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Boundary-layer transition and displacement-thickness effects on zero-lift drag of a series of power-law bodies at Mach 6 /

Ashby, George C.
Harris, Julius E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

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 ...

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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

Penland, Jim A.
Pittman, Jimmy L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."August 1985"--Cover.Includes bibliographical references (p. 10)...

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: ...

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

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 ...

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Reubush, David E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 8-9).Mode of access: Internet

Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model /

Hoad, Danny R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Boundary-layer transition and displacement-thickness effects on zero-lift drag of a series of power-law bodies at Mach 6 /

Ashby, George C.
Harris, Julius E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

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 ...

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

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

Penland, Jim A.
Pittman, Jimmy L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."August 1985"--Cover.Includes bibliographical references (p. 10)...

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: ...

Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wing /

Ray, Edward J.
Taylor, Robert T., NASA researcher.
Langley Research Center.

January 1967

"NASA TM X-1386.""Langley Research Center, Langley Station, Hampton, Va.""June 1967"--Cover.Includes...

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 ...

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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...

Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /

Reubush, David E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 8-9).Mode of access: Internet

Longitudinal aerodynamic characteristics of a deflected-thrust propulsive-lift transport model /

Hoad, Danny R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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