Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity /

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

Effects of coupling between pitch and roll control inputs on the handling qualities of VTOL aircraft /

Garren, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stability and control.Includes bibliographical references.Mode of access: I...

A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft /

Gerdes, Ronald M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aircraft; Simulators and computers; Stability and control.Includes bibli...

Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence /

Tosti, Louis P.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

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

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...

Longitudinal trim characteristics of a deflected slipstream V/Stol aircraft during level flight at transition flight speeds / Howard L. Turner and Fred J. Drinkwater III.

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator /

Vomaske, Richard F.
Drinkwater, Fred J.
Sadoff, Melvin
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; St...

Some flight characteristics of a deflected slipstream V/STOL aircraft /

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

Effects of coupling between pitch and roll control inputs on the handling qualities of VTOL aircraft /

Garren, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stability and control.Includes bibliographical references.Mode of access: I...

A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft /

Gerdes, Ronald M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aircraft; Simulators and computers; Stability and control.Includes bibli...

Lateral control characteristics of a powered model of a twin-propeller deflected slipstream STOL airplane configuration

Margason, Richard J.
Hammond, Alexander D.
United States. National Aeronautics and Space Administration.

Cover title."November 1964."Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

Aerodynamic characteristics of a 1/4-inch scale model a tilt-wing VTOL aircraft at high angles of wing incidence /

Tosti, Louis P.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

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...

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Low speed static longitudinal and lateral aerodynamic characteristics of a model with a low-aspect-ratio variable-incidence wing and with a free-floating and a programed high-lift canard control /

Scallion, William I.
United States. National Aeronautics and Space Administration.

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

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...

Longitudinal trim characteristics of a deflected slipstream V/Stol aircraft during level flight at transition flight speeds / Howard L. Turner and Fred J. Drinkwater III.

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator /

Vomaske, Richard F.
Drinkwater, Fred J.
Sadoff, Melvin
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; St...

Some flight characteristics of a deflected slipstream V/STOL aircraft /

Turner, Howard L.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

Effects of coupling between pitch and roll control inputs on the handling qualities of VTOL aircraft /

Garren, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stability and control.Includes bibliographical references.Mode of access: I...

A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft /

Gerdes, Ronald M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aircraft; Simulators and computers; Stability and control.Includes bibli...

Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity /

Abstract

Extracted data

Lateral stability and control characteristics of a four-propleer deflected-slipstream VTOL model inculding the effects of ground proximity /

Abstract

Extracted data

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