Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans /

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...

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 ...

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 ...

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

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...

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Loving, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and ...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Aerodynamic characteristics in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a mach number of 2.01 /

Robinson, Ross B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers; S...

Investigation of interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model /

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

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Propulsion sys...

Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform /

Landrum, Emma Jean.
Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control.In...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

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...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

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...

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 ...

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 ...

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

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...

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Loving, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and ...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Aerodynamic characteristics in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a mach number of 2.01 /

Robinson, Ross B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, missiles and space vehicles; Missiles and satellite carriers; S...

Investigation of interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model /

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

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Propulsion sys...

Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform /

Landrum, Emma Jean.
Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control.In...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

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...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

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...

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 ...

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 ...

Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans /

Abstract

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Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans /

Abstract

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