Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

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

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle /

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; Simula...

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...

A theoretical investigation of the effect of cross-control derivatives on the stability characteristics of airplanes designed for flight at high mach numbers /

Brown, Lawrence W.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

A flight study of the conversion maneuver of a tilt-duct VTOL aircraft /

Tapscott, Robert J.
Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Flight controllability limits and related human transfer functions as determined from simulator and flight tests /

Taylor, Lawrence W.
Day, Richard E.
United States. National Aeronautics and Space Administration.

Cover title." May 1961."Aerodynamics, aircraft; Aircraft; Simulators and computers;Stability and con...

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

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

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle /

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; Simula...

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...

A theoretical investigation of the effect of cross-control derivatives on the stability characteristics of airplanes designed for flight at high mach numbers /

Brown, Lawrence W.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Force-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Wind-tunnel investigation of a small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

A flight study of the conversion maneuver of a tilt-duct VTOL aircraft /

Tapscott, Robert J.
Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Flight controllability limits and related human transfer functions as determined from simulator and flight tests /

Taylor, Lawrence W.
Day, Richard E.
United States. National Aeronautics and Space Administration.

Cover title." May 1961."Aerodynamics, aircraft; Aircraft; Simulators and computers;Stability and con...

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

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

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

Abstract

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Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

Abstract

Extracted data

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