Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

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...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /

Gloss, Blair B.
Langley Research Center.

January 1974

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

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

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

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of canard location and size on canard-wing interference and aerodynamic center shift related to maneuvering aircraft at transonic speeds

Gloss, B. B.

June 1974

A generalized wind-tunnel model, typical of highly maneuverable aircraft, was tested in the Langley ...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing /

Mineck, Raymond E.
Carter, Arthur W.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

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 ...

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

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 ...

A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft /

Keith, Arvid L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

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...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /

Gloss, Blair B.
Langley Research Center.

January 1974

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

Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds /

Gloss, Blair B.
Langley Research Center.

January 1975

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

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 ̊sweptback wing at a Mach number of 0.30 /

Henderson, William P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Effect of canard location and size on canard-wing interference and aerodynamic center shift related to maneuvering aircraft at transonic speeds

Gloss, B. B.

June 1974

A generalized wind-tunnel model, typical of highly maneuverable aircraft, was tested in the Langley ...

Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing /

Mineck, Raymond E.
Carter, Arthur W.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

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 ...

Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

Pittman, Jimmy L.
Mason, William H. (William Henry), 1947-
Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

"February 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical re...

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 ...

A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft /

Keith, Arvid L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

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...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /

Abstract

Extracted data

Effect of canard location and size on canard-wing interference and aerodynamic-center shift related to maneuvering aircraft at transonic speeds /

Abstract

Extracted data

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