Flight Training Central
MARCH 3, 2025
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.
Pilot Institute
JUNE 4, 2025
Use of Reflex Airfoils Ever notice how many tailless aircraft have wings that curve at the trailing edge? This type of design is a reflex airfoil. The reflexed shape of the airfoil usually causes a positive (nose-up) pitching moment coefficient at its aerodynamic center. They combine the functions of elevators and ailerons.
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Pilot Institute
MARCH 28, 2025
When air flows over the aircraft wing, the shape of the airfoil creates low pressure above the wing and relatively higher pressure below the wing. When the aircraft encounters a vortex and its strong enough to induce roll, the pilot counters it by using the ailerons against the roll and tries to fly out of the wake as soon as possible.
Vintage Aviation News
APRIL 18, 2025
Photo by NASA The impetus for the program came from issues the Navy had encountered with inadvertent spin entries, which were traced back to the aircrafts aileron rudder interconnect system. These glove modifications served to smooth the wing surface and alter the airfoil to achieve specific pressure distributions.
Pilot Institute
FEBRUARY 9, 2025
Wing Control: Flaps, slats, and ailerons change the chord line, impacting lift and control. In general, the chord line is used as an easy-to-understand reference when referring to the properties of a wing or airfoil. Basically, the mean camber line is meant to indicate the midpoint between the top and bottom surfaces of the airfoil.
Vintage Aviation News
APRIL 1, 2025
The delta wing’s large area (425 square feet), thin airfoil cross section, low weight, and structural strength made a great combination for a supersonic aircraft. It was controlled by a conventional rudder and full-span elevons that functioned as elevators and ailerons. The XF-92A was then used to test the delta-wing concept.
Pilot Institute
JULY 11, 2025
Making the wing relatively flat on top with a blunter leading edge and more curvature on the bottom gives you a supercritical airfoil. Ailerons can suffer from a phenomenon called “aileron buzz” or control reversal at high Mach. Even the wing cross-section can be designed to redirect shock waves. roughly) up to about Mach 5.0.
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