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

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Structural-loads surveys on two tilt-wing VTOL configurations /

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

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane /

Quigley, Hervey C.
Koenig, David G.
United States. National Aeronautics and Space Administration.

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

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

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 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...

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 ...

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...

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-45.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

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

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...

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...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

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...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Structural-loads surveys on two tilt-wing VTOL configurations /

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

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane /

Quigley, Hervey C.
Koenig, David G.
United States. National Aeronautics and Space Administration.

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

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

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 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...

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 ...

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...

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-45.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

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

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...

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...

Aerodynamics of a tilting ducted fan configuration /

Yaggy, Paul F.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet; Stability an...

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...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Structural-loads surveys on two tilt-wing VTOL configurations /

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

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane /

Quigley, Hervey C.
Koenig, David G.
United States. National Aeronautics and Space Administration.

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

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

Abstract

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

Abstract

Extracted data

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