Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

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

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

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

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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 ...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

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

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...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

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

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently /

Barger, Raymond L.
Langley Research Center.

January 1974

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

Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft /

O'Connell, Robert F.
Radovcich, N. A., joint author.
Hassig, H. J., joint author.
Lockheed-California Company.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 115-117).Mode of access: Internet

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

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 ...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

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

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...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

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

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

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Abstract

Extracted data

Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios /

Abstract

Extracted data

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