Notes on the Stalling of Vertical Tail Surfaces and on Fin Design PDF Download
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Author: F. L. Thompson Publisher: ISBN: Category : Airplanes Languages : en Pages : 566
Book Description
It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.
Author: F. L. Thompson Publisher: ISBN: Category : Airplanes Languages : en Pages : 566
Book Description
It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.
Author: James C. Williams Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 716
Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Author: Frederick H. Imlay Publisher: ISBN: Category : Airplanes Languages : en Pages : 546
Book Description
The lateral motion resulting from a disturbance of the type produced by asymmetric loss of thrust has been determined for a hypothetical average airplane equipped with an automatic pilot. Plots of the resultant motion and the various modes that constitute the motion are presented for controls fixed and for various amounts of automatic control. The automatic control is assumed to be of a type that produces aileron deflections proportional to the angle of bank and rudder deflections proportional to the angle of azimuth. The use of an automatic control may introduce either of two modes. The first mode is primarily a rolling oscillation; the second is a poorly damped long-period oscillation in azimuth and bank . The motion following any change in trim causes the airplane to reach a state of equilibrium on a different flight heading from that existing before the disturbance and the airplane assumes a new flight attitude.
Author: F. L. Thompson
Author: F. L. Thompson
Author: United States. National Advisory Committee for Aeronautics
Author: Royal Aeronautical Society
Author: Virginia Parker Dawson
Author: United States. National Advisory Committee for Aeronautics
Author: James C. Williams
Author: University of Michigan. Engineering Summer Conferences
Author: 
Author: Frederick H. Imlay
Author: United States. National Advisory Committee for Aeronautics