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Krueger flaps deployed from the leading edge of a Boeing 747 (top left and right in photo). Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. Unlike slats or droop flaps, the main wing upper surface and its nose is not changed. Instead, a portion of the lower wing is ...
CrawTrawler. Is cutting 10% of its workforce, impacting roughly 40 employees. The company, however, said it will create 28 new roles as part of its new strategy. ApplyBoard. Has eliminated 4% of ...
In aerodynamics, the torques or moments acting on an airfoil moving through a fluid can be accounted for by the net lift and net drag applied at some point on the airfoil, and a separate net pitching moment about that point whose magnitude varies with the choice of where the lift is chosen to be applied. The aerodynamic center is the point at ...
Spar (aeronautics) In a fixed-wing aircraft, the spar is often the main structural member of the wing, running spanwise at right angles (or thereabouts depending on wing sweep) to the fuselage. The spar carries flight loads and the weight of the wings while on the ground. Other structural and forming members such as ribs may be attached to the ...
Nike Men's InfinityRN4. $97$160Save $63. Nike makes some of the best sneakers on the market, and during Labor Day, you can get this pair of Nike InfinityRN4 running shoes up to 39% off. If you use ...
Peloton, the exercise equipment maker and online fitness course provider, said it is laying off 15% of its workforce (about 400 people) as part of cost-cutting measures. The company also said its ...
Previously, the company had followed Apple’s move by reducing commissions from 30% to 15% on the first $1 million of developer earnings. Now, it will lower the fees specifically for app makers ...
For example, the NACA 23112 profile describes an airfoil with design lift coefficient of 0.3 (0.15 × 2), the point of maximum camber located at 15% chord (5 × 3), reflex camber (1), and maximum thickness of 12% of chord length (12). The camber line for the simple case (S = 0) is defined in two sections: [11]
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