Airfoil Drag Lift 
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. This is called lift. Wingtip vortices are a byproduct of lift. Once the wing stops producing lift, the vortices dissipate instantly. How Are Wingtip Vortices Formed?
Pilot Institute
MARCH 13, 2025
Many explanations on websites, videos, and even some textbooks oversimplify or misrepresent the true mechanics of lift. In reality, lift generation involves both Bernoullis principle and Newtons third law working together. Read on to understand Bernoullis principle and how it relates to lift the right way.
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Vintage Aviation News
APRIL 1, 2025
Studying historical aircraft helps students understand the development of flight and learn from early engineers about problems of lift, propulsion, stability, and material constraints. Often touted as the first successful powered aircraft, the Wright Flyer (1903) clearly shows lift, propulsion, and control.
Flight Training Central
MAY 7, 2024
The term 'angle of attack' is defined as the angle between the airplane's longitudinal axis and that of the air striking the airfoil. Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface. The horizontal component of lift. The vertical component of lift.
Vintage Aviation News
DECEMBER 29, 2024
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 Davis Wing allowed for higher speeds and added lift at relatively low angles of attack.
Vintage Aviation News
APRIL 11, 2025
They flew a total of 313 missions, collecting invaluable data on pitch stability, lift, drag, and buffeting in transonic and supersonic flight. The jet- and rocket-powered aircraft exceeded expectations, performing better than predicted in high-speed wind tunnel testsparticularly in drag performance above Mach 0.85.
Vintage Aviation News
OCTOBER 7, 2024
The unique cylindrical design of the fuselage allowed for a streamlined profile and reduced drag, increasing the overall efficiency. During these years, he concluded that the inner surface of the venturi tube needed an airfoil shape to achieve the greatest efficiency. The Stipa-Caproni in flight.
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