Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

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...

The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraft /

Szalai, Kenneth J.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 45).Mode of access: Internet

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

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

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

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

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

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

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

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

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...

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...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

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...

The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraft /

Szalai, Kenneth J.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 45).Mode of access: Internet

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

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

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

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

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

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

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

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

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...

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...

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

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...

The influence of response feedback loops on the lateral-directional dynamics of a variable-stability transport aircraft /

Szalai, Kenneth J.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 45).Mode of access: Internet

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

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

Abstract

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Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

Abstract

Extracted data

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