Remove Drag Remove Lift Remove Runway
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EASA certifies modified Airbus A330neo with enhanced bonus features 

Aerotime

This is achieved by further maximizing lift and reducing drag during the take-off and initial climb segments, a spokesperson for Airbus said. At other, even more runway-restricted airports, the net gain could be as much as seven tons without increasing the engines thrust, added the spokesperson.

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Powered-Lift Specialist XTI Explores Uncrewed, Magnetically Powered Aircraft

Flying Magazine

This prevents tip vortices—a phenomenon where air leaks around blade tips, causing thrust loss and increased drag. The company further claims it can achieve the same lift as an eVTOL with significantly lower tip speed and revolutions per minute. It could even enable short takeoff and landing (STOL) from the runway.

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Wingtip Vortices and Wake Turbulence

Pilot Institute

This is called lift. Wingtip vortices are a byproduct of lift. Once the wing stops producing lift, the vortices dissipate instantly. Wing spoilers drastically reduce the lift generated by the wing. Its important because the lift is always produced perpendicular to the relative wind. Why is this important?

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Going Up and Going Down

Plane and Pilot

When discussing climb technique, it’s easy to confuse high power setting with increasing lift. It’s the wing that generates lift, not the engine. This climb speed is determined by minimizing the two sources of drag acting against the airplane. Although optimum, V Y is simply in the middle of a fairly broad lift-over-drag curve.

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5 Most Common Aircraft Flap Types (Explained by a CFI)

Northstar VFR

When deployed, they increase the wings lift and drag, allowing the airplane to fly safely at slower speeds. When flaps extend, they increase the camber (curvature) of the wing, which boosts the amount of lift the wing generates. At the same time, flaps create extra drag, which helps slow the airplane down.

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Step-by-Step Guide to No-Flaps Landings for Pilots

Pilot Institute

Flatter approach angle (due to less drag). A no-flaps landing generally requires more runway for stopping, with the distance that can increase by as much as 50% depending on the aircraft and conditions. In such a situation, you need to maintain lift by adjusting the angle of attack and airspeed, which requires precise control.

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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 Davis Wing allowed for higher speeds and added lift at relatively low angles of attack.