The determination of the topological structure of skin friction lines on a rectangular wing-body combination /

Theory for computing the field scattered from a smooth inflected surface /

Barger, Raymond L.
Dominek, Allen K.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 1...

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...

Advances in contact algorithms and their application to tires /

Noor, Ahmed Khairy, 1938-
Tanner, John A.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 15-1...

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

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

Shape sensitivity analysis of wing static aeroelastic characteristics /

Barthelemy, Jean-Francois M.
Bergen, Fred D.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 18).Mo...

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

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).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

Computational methods for frictionless contact with application to space shuttle orbiter nose-gear tires /

Kim, Kyun O.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 15.Mode of access: Internet

A method for the design of transonic flexible wings /

Smith, Leigh Ann.
Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 14.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...

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

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 ...

Theory for computing the field scattered from a smooth inflected surface /

Barger, Raymond L.
Dominek, Allen K.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 1...

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...

Advances in contact algorithms and their application to tires /

Noor, Ahmed Khairy, 1938-
Tanner, John A.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 15-1...

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

Kuhlmann, John, 1948-
Cerney, Michael J.
Liaw, Paul.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

Prepared for Langley Research Center under Grant NAG1-625."August 1988"--Cover.Bibliography: p. 34-3...

Shape sensitivity analysis of wing static aeroelastic characteristics /

Barthelemy, Jean-Francois M.
Bergen, Fred D.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 18).Mo...

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

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).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

Computational methods for frictionless contact with application to space shuttle orbiter nose-gear tires /

Kim, Kyun O.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 15.Mode of access: Internet

A method for the design of transonic flexible wings /

Smith, Leigh Ann.
Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 14.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...

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

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 ...

Theory for computing the field scattered from a smooth inflected surface /

Barger, Raymond L.
Dominek, Allen K.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 1...

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...

Advances in contact algorithms and their application to tires /

Noor, Ahmed Khairy, 1938-
Tanner, John A.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 15-1...

The determination of the topological structure of skin friction lines on a rectangular wing-body combination /

Abstract

Extracted data

The determination of the topological structure of skin friction lines on a rectangular wing-body combination /

Abstract

Extracted data

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