Remove Airfoil Remove Drag Remove Stability
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Today in Aviation History: First Flight of the Stipa-Caproni

Vintage Aviation News

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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Recognising NASA Technology on Modern Airliners

Fear of Landing

One of the most revolutionary was the “area rule,” a concept that helped aircraft designers avoid the disruption in airflow and resulting drag caused by the attachment of the wings to the fuselage. The resulting “supercritical airfoil” shape, when integrated with the aircraft wing, significantly improves the aircraft’s cruise efficiency.

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The Hazards of Aircraft Icing: Explained

Pilot Institute

And ice doesn’t just make things slippery, it messes with the airflow over the wings, cuts down on lift, and ramps up drag. Remember that wings, propeller blades, and tail surfaces are airfoil-shaped. Ice build-up on the airframe changes the airflow pattern around these airfoils.

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Today in Aviation History: First Flight of the Kawanishi E15K

Vintage Aviation News

Additionally, the Shiun incorporated a laminar flow airfoil to reduce drag. However, this would mean that the Shiun’s pilot would have to ditch the aircraft in the water, with the stabilizing floats deploying to add buoyancy to the aircraft. But there were also several key distinctions between the Kyofu and the Shiun.

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Nothing Small About It

Plane and Pilot

Winging It Aside from the aforementioned desire for a greater aspect ratio for reduced drag, the one-piece Gweduck wing was developed for minimal weight, ease of construction and benign handling. Keeping drag corralled was emphasized as the Gweduck mission is foremost long-distance cruising.

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Return to Form

Plane and Pilot

For one thing, the F2s fuselage hangs from a completely new wing with two distinct airfoil shapes. An obvious discontinuity leads to a thinner airfoil inboard. The previous CTs had a stabilator for pitch, where the new F2 uses a more conventional elevator and fixed horizontal stabilizer.

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