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Today in Aviation History: First Flight of the Consolidated B-24 Liberator

Vintage Aviation News

Davis, who had developed a new wing, whose airfoil had a lower drag co-efficiency than other wing designs of the time, and which had already been used on the company’s Model 31/XP4Y Corregidor flying boat. The company had hired a freelance aeronautical engineer, David R.

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Tailless Aircraft: How Airplanes Fly Without a Tail

Pilot Institute

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. Flying wings dont have tails or elevators.

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What Is Bernoulli’s Principle? A Simple Guide for Pilots

Pilot Institute

Airfoils use this principle, with faster airflow over the top creating lower pressure. If lift were entirely due to Bernoulli, a symmetric airfoil (one with equal curvature on top and bottom) wouldnt generate lift – yet it does when given the right angle of attack. In reality, the wing also uses Newtons third law to create lift.

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Flight Test Files: The Douglas D-558-2 Skyrocket – Chasing Mach 2

Vintage Aviation News

Both aircraft display early examples of swept-wing airfoils. The Skyrocket also contributed to refining wind tunnel methodologies and validating theories of flight dynamics in the transonic and supersonic regimes. This 1950s photograph shows the Douglas D-558-2 and the North American F-86 Sabre chase aircraft in flight.

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Wingtip Vortices and Wake Turbulence

Pilot Institute

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. Wake turbulence can cause severe roll and structural damage to smaller aircraft. Pilots avoid vortices by maintaining safe separation and adjusting flight paths. How Are Wingtip Vortices Formed?

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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. While its extremely important to understand what conditions can lead to a stall, how to recognize an impending stall, and correct recovery techniques, its not something to fear during your everyday flying.

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Flight Test Files: Grumman F-14 Tomcat

Vintage Aviation News

These glove modifications served to smooth the wing surface and alter the airfoil to achieve specific pressure distributions. For the VSTFE program, the outer wing panels of NASA 834 were fitted with specially designed natural laminar flow gloves.