Analysis of transonic flow about lifting wing-body configurations /

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

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

January 1974

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

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 ...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

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 ...

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 ...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

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

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 ...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

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

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...

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...

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 ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

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

January 1974

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

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 ...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

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 ...

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 ...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

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

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 ...

Lee-side flow over delta wings at supersonic speeds /

Miller, David S.
Wood, Richard M.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 150)....

Calculative techniques for transonic flows about certain classes of wing-body combinations /

Stahara, Stephen S.
Spreiter, John R.
Ames Research Center.
Nielsen Engineering & Research.

January 1972

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

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

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...

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...

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 ...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

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

January 1974

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

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 ...

Analysis of transonic flow about lifting wing-body configurations /

Abstract

Extracted data

Analysis of transonic flow about lifting wing-body configurations /

Abstract

Extracted data

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