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  2. Swept wing - Wikipedia

    en.wikipedia.org/wiki/Swept_wing

    The angle needed to lie behind the cone increases with increasing speed, at Mach 1.3 the angle is about 45 degrees, at Mach 2.0 it is 60 degrees. [10] The angle of the Mach cone formed off the body of the aircraft will be at about sin μ = 1/M (μ is the sweep angle of the Mach cone). [11]

  3. Forward-swept wing - Wikipedia

    en.wikipedia.org/wiki/Forward-swept_wing

    One problem with the forward-swept design is that when a swept wing yaws sideways (moves about its vertical axis), one wing retreats while the other advances. On a forward-swept design, this reduces the sweep of the rearward wing, increasing its drag and pushing it further back, increasing the amount of yaw and leading to directional instability.

  4. Sukhoi Su-17 - Wikipedia

    en.wikipedia.org/wiki/Sukhoi_Su-17

    With wings at maximum sweep, the Su-17 would look virtually identical to the Su-7. A slide-out flap was installed on the stationary part of the wing, while a slat, a rotating flap and aileron were mounted on the rotating part. The sweep angle could be configured between 30° and 63°. The horizontal and vertical tails were swept at 55°.

  5. Oblique wing - Wikipedia

    en.wikipedia.org/wiki/Oblique_wing

    By changing its sweep angle in this way, drag can be reduced at high speed (with the wing swept) without sacrificing low speed performance (with the wing perpendicular). This is a variation on the classic swing-wing design , intended to simplify construction and retain the center of gravity as the sweep angle is changed.

  6. Wing configuration - Wikipedia

    en.wikipedia.org/wiki/Wing_configuration

    This helps avoid tip drag at high angles of attack. The Fairey Delta 1 also had a tail. At the extreme, merges into the "tapered swept" configuration. Compound delta or double delta: inner section has a (usually) steeper leading edge sweep as on the Saab Draken. This improves the lift at high angles of attack and delays or prevents stalling.

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  8. Variable-sweep wing - Wikipedia

    en.wikipedia.org/wiki/Variable-sweep_wing

    A variable-sweep wing allows the pilot to use the optimum sweep angle for the aircraft's speed at the moment, whether slow or fast. The more efficient sweep angles available offset the weight and volume penalties imposed by the wing's mechanical sweep mechanisms. Its greater complexity and cost make it practical mostly for military aircraft.

  9. Your Grandmother Never Made This Pimiento Cheese Mistake, And ...

    www.aol.com/grandmother-never-made-pimiento...

    Southerners have a lot of rules when it comes to cooking—and some of them are subjective. For example, some folks simply abhor putting sugar in cornbread, washing their cast-iron skillet with ...