Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

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...

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets /

Whitcomb, Richard T.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method /

Mann, Michael J.
Mercer, Charles E.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 2...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges /

Carlson, Harry W.
Darden, Christine M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 14...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /

Goradia, Suresh H. (Suresh Harkisondas), 1937-
Lilley, D. G.
Langley Research Center.
Lockheed-Georgia Company.

"Prepared by Lockheed-Georgia Company ... for Langley Research Center.""June 1975."Cover title.Inclu...

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 ...

Flutter of a low-aspect-ratio rectangular wing /

Cole, Stanley R.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5.Mode of access: Internet

Effects of winglets on first-generation jet transport wing /

Flechner, Stuart G.
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.v. 6. Stability ...

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...

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets /

Whitcomb, Richard T.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method /

Mann, Michael J.
Mercer, Charles E.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 2...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

Natural laminar flow airfoil design considerations for winglets on low-speed airplanes /

Van Dam, C. P. (Cornelis P.), 1954-
Langley Research Center.
Vigyan Research Associates.

January 1984

"Prepared [at Vigyan Research Associates] for Langley Research Center under Contract NAS1-17797.""De...

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...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

Subsonic annular wing theory with application to flow about nacelles /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 90-91).Mode ...

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges /

Carlson, Harry W.
Darden, Christine M.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 14...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /

Goradia, Suresh H. (Suresh Harkisondas), 1937-
Lilley, D. G.
Langley Research Center.
Lockheed-Georgia Company.

"Prepared by Lockheed-Georgia Company ... for Langley Research Center.""June 1975."Cover title.Inclu...

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 ...

Flutter of a low-aspect-ratio rectangular wing /

Cole, Stanley R.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5.Mode of access: Internet

Effects of winglets on first-generation jet transport wing /

Flechner, Stuart G.
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.v. 6. Stability ...

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...

A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets /

Whitcomb, Richard T.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method /

Mann, Michael J.
Mercer, Charles E.
Langley Research Center.

January 1986

Prepared at Langley Research Center."November 1986"--Cover.Includes bibliographical references (p. 2...

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Abstract

Extracted data

Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag /

Abstract

Extracted data

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