Remove Drag Remove Lift Remove Stability
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Tailless Aircraft: How Airplanes Fly Without a Tail

Pilot Institute

A tailless aircraft is a fixed-wing airplane without a horizontal stabilizing surface. With this type of aircraft, the functions of longitudinal stability and control are incorporated into the main wing. A tailless airplane is one where everything needed to fly, like lift, control, and stability, is built into the main wing.

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Learning Aeronautical Engineering From Historic Aircraft Designs

Vintage Aviation News

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.

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

Vintage Aviation News

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.

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What are the Key Parts of a Plane?

WayMan

Wings: The Source of Lift The wings are what make fixed-wing flight possible. As air moves over the curved top surface of the wing and the flatter bottom, lift is generated, allowing the plane to rise. Regardless of placement, the principle remains the same: wings generate the lift that makes flight possible.

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Airspeed and Altitude Control Simplified: Tips for Stable Flying

Pilot Institute

The faster an aircraft goes, the more lift it generates. Lift is the upward force that keeps you in the air. If airspeed is too slow, the aircraft could lose lift and stall. Meanwhile, lower altitudes demand that you be extra careful with airspeed to maintain lift and prevent stalls. miles per hour.

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Throttle Mismanagement: A T-38 Lesson That Stuck

Air Facts

As he lifted off from a touch-and-go, I shook the control stick and said, Ive got the jet. At pattern altitude, I leveled off, and our airspeed stabilized at 300 KIAS. The G-loading and added drag slowed us below the gear limit speed (240 KIAS). I wanted him to make minor correctionsand only when necessary.

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Flight Test Files: B-47A Stratojet

Vintage Aviation News

Langley was particularly focused on structural loads, while Ames concentrated on dynamic stability. Although the B-47A appeared structurally sound upon arrival, flight testing revealed notable shortcomingsparticularly buffeting issues that limited both its top speed and achievable lift. The average gross weight was 115,000 pounds.