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Mastering Stalls: How to Recognize, Prevent, and Recover Safely

Flight Training Central

Depending on design, airfoils used in general aviation, stall at angles of attack between 16 to 18 degrees. Recovery is made by lowering the nose, simultaneously applying full power while maintaining directional control with coordinated use of aileron and rudder. The recovery procedure is the same as for all stalls.

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Everything You Need To Know About Ailerons

Pilot Institute

Adverse yaw is a side effect of aileron use, countered by rudder input. In recent times, composite materials have been introduced for flight controls even in small general aviation aircraft. Fly-by-wire is expensive, so you wont find it on most small general aviation aircraft. What Is an Aileron?

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The Role of Newton’s Third Law in Aviation

Pilot Institute

High camber generally promotes more airflow deflection, thanks to something called Bernoullis Principle. This is why the typical airfoil shape has a curved top and a flat bottom, especially in slower-speed general aviation aircraft. Other Designs The tail rotor is not the only way to solve the torque reaction problem.

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Nothing Small About It

Plane and Pilot

Another advantage of the counter-rotating props is the elimination of torque roll. This is the tendency to dig in the left tip float during takeoff while countering engine torque. An elegantly simple rope system inside the fuselage raises and lowers the Gweduck’s water rudder mounted inside the base of the main rudder (right).