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

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...

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 ...

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Martin, Fred W., author.
Cutchins, Malcolm A., author.
Saunders, Grady. Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Auburn University. Department of Aerospace Engineering. sponsor.

"April 1976."Includes bibliographical references (page 47).Print reproduction.Air Force Contract No....

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

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).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...

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

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

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

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...

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...

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...

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

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...

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...

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...

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 ...

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Martin, Fred W., author.
Cutchins, Malcolm A., author.
Saunders, Grady. Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Auburn University. Department of Aerospace Engineering. sponsor.

"April 1976."Includes bibliographical references (page 47).Print reproduction.Air Force Contract No....

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

Spreemann, Kenneth P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).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...

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

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

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

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...

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...

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...

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

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...

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...

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...

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 ...

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Martin, Fred W., author.
Cutchins, Malcolm A., author.
Saunders, Grady. Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Auburn University. Department of Aerospace Engineering. sponsor.

"April 1976."Includes bibliographical references (page 47).Print reproduction.Air Force Contract No....

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

Abstract

Extracted data

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

Abstract

Extracted data

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