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

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...

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...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

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

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

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...

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...

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...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Wind-tunnel tests of a 1/20-scale airship model with stern propellers /

McLemore, H. Clyde.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Stability and control;Includes bibliographical re...

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...

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. /

Koenig, David G.
Brady, James A.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Experimental investigation of some of the parameters related to the stability and control of aerial vehicles supported by ducted fans /

Parlett, Lysle P.

Three investigations, all related to the stability and control characteristics of ducted-fan aerial ...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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...

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...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

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

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

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...

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...

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...

Low-speed wind-tunnel investigation to determine the flight characteristics of a model of a parawing utility vehicle. Joseph L. Johnson.

Johnson, Joseph L.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogra...

Wind-tunnel tests of a 1/20-scale airship model with stern propellers /

McLemore, H. Clyde.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Stability and control;Includes bibliographical re...

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...

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

Large-scale wind-tunnel tests of a wingless vertical take-off and landing aircraft - preliminary results. /

Koenig, David G.
Brady, James A.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliogr...

Experimental investigation of some of the parameters related to the stability and control of aerial vehicles supported by ducted fans /

Parlett, Lysle P.

Three investigations, all related to the stability and control characteristics of ducted-fan aerial ...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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...

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...

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

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

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

Abstract

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

Abstract

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