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

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:...

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

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...

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...

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. ...

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...

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...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes 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...

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...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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...

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /

Carlson, Harry W.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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:...

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

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...

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...

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. ...

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...

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...

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations /

Paulson, John W.
Thomas, James L. (James Lee), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""December 1979"-- CoverIncludes 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...

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...

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

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...

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /

Carlson, Harry W.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Effect of under-wing aft-mounted nacelles on the longitudinal aerodynamic characteristics of a high-wing transport airplane /

Abeyounis, William Kelly.
Patterson, James C.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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:...

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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