Handling qualities experience with several VTOL research aircraft /

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

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

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Operational experiences of turbine-powered commercial transport airplanes /

United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Aircraft safety and noise; Piloting; Stresses and loads; Struct...

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...

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 ...

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

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...

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...

Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft /

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

Cover title."April 1961."Simulators and computers;Stability and control;Vehicle performance;Includes...

Operational technique for transition of several types of V/STOL aircraft /

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

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

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

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

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

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

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

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...

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...

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...

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

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

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

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Operational experiences of turbine-powered commercial transport airplanes /

United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Aircraft safety and noise; Piloting; Stresses and loads; Struct...

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...

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 ...

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

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

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

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...

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...

Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft /

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

Cover title."April 1961."Simulators and computers;Stability and control;Vehicle performance;Includes...

Operational technique for transition of several types of V/STOL aircraft /

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

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

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

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

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

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

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

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...

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...

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...

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

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

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

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Operational experiences of turbine-powered commercial transport airplanes /

United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Aircraft safety and noise; Piloting; Stresses and loads; Struct...

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...

Handling qualities experience with several VTOL research aircraft /

Abstract

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Handling qualities experience with several VTOL research aircraft /

Abstract

Extracted data

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