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

Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /

Mann, Michael J.
Campbell, Richard L. (Richard Lawson), 1952-
Mercer, Charles E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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...

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...

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...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

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...

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...

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...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

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

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:...

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /

Mann, Michael J.
Campbell, Richard L. (Richard Lawson), 1952-
Mercer, Charles E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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...

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...

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...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

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...

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...

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...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

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

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:...

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20 /

Gillespie Jr., Warren.
Langley Research Center.

Prepared at the Langley Research Center, Langley Field, VA.Cover title."October 1960."--Cover.Includ...

Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 /

Mann, Michael J.
Campbell, Richard L. (Richard Lawson), 1952-
Mercer, Charles E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"September 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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...

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

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

Abstract

Extracted data

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

Abstract

Extracted data

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