22 research outputs found
Floating Characteristics of Rudders and Elevators in Spinning Attitudes as Determined from Hinge-moment-coefficient Data with Application to Personal-owner-type Airplanes
Get PDFAnalytical studies of the response to longitudinal control of three airplane configurations in landing approaches
Get PDFThe Aerodynamic Forces and Moments on a 1/10-scale Model of a Fighter Airplane in Spinning Attitudes as Measured on a Rotary Balance in the Langley 20-foot Free-spinning Tunnel
Get PDF
Recommended from our members
NACA Technical Notes
No full textReport presenting an investigation to determine the floating characteristics of full-length plain and horn-balanced rudders during rotary tests at spinning attitudes on a scale model of a typical low-wing personal-owner airplane. The investigation included the determination of the effects of the horizontal tail and the wing on the rudder floating characteristics
Recommended from our members
NACA Technical Notes
No full textReport presenting a study of the available rudder and elevator hinge-moment-coefficient data in order to determine the floating characteristics of various types of rudders and elevators in spinning attitudes. Results regarding the rudder floating characteristics, elevator floating characteristics, and a comparison of several types of rudders and elevators are provided
Departure susceptibility and uncoordinated roll-reversal boundaries for fighter configurations
No full textInfluence of the Static and Dynamic Aerodynamic Characteristics on the Spinning Motion of Aircraft
No full textRecommended from our members
NACA Research Memorandums
No full textFrom Introduction: "A theoretical investigation was conducted in order to determine what effect the differences in aerodynamic characteristics would have on the short-time response to elevator control of this type of airplane as compared with the responses of a conventional airplane, without regard to any possible psychological influences. The results of this investigation are presented in this paper.
