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

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).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

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

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...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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

Gloss, Blair B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).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

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

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...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

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

Gloss, Blair B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails /

Peterson, Victor L.
United States. National Aeronautics and Space Administration.

Cover title." June 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

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

Abstract

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

Abstract

Extracted data

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