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Supercritical airfoils feature four main benefits: they have a higher drag-divergence Mach number, [21] they develop shock waves farther aft than traditional airfoils, [22] they greatly reduce shock-induced boundary layer separation, and their geometry allows more efficient wing design (e.g., a thicker wing and/or reduced wing sweep, each of which may allow a lighter wing).
Using this method, supercritical wings were fabricated and proven on full-scale aircraft; in 1971 a Vought F-8 Crusader, and in 1973 a General Dynamics F-111 Aardvark, were flown at the NASA Flight Research Center in California. For his contribution, NASA awarded Whitcomb a $25,000 prize, and he received the 1974 Wright Brothers Memorial Trophy ...
Design of the Gulfstream III started with an effort to synthesize a completely new wing employing NASA supercritical airfoil sections and winglets. Optimization studies considering weight, drag, fuel volume, cost, and performance indicated that a substantial portion of the new wing benefit could be secured with modifications to the existing wing.
Precision Castparts Corp. is an American industrial goods and metal fabrication company that manufactures investment castings, forged components, and airfoil castings for use in the aerospace, industrial gas turbine, and defense industries. In 2009 it ranked 362nd on the Fortune 500 list, and 11th in the aerospace and defense industry. [3]
Here's what else happened today: Disney said it will appoint Bob Iger's successor as CEO by early 2026. Goldman Sachs said investors should prepare for a decade of muted returns in the stock market.
U.S. stocks closed broadly lower Monday as a banner year on Wall Street looked set to finish on a sour note. The S&P 500 fell 1.1%, its third straight decline. Roughly 90% of stocks within the ...
The supercritical airfoil is a type that results in reasonable low speed lift like a normal airfoil, but has a profile considerably closer to that of the von Kármán ogive. All modern civil airliners use forms of supercritical aerofoil and have substantial supersonic flow over the wing upper surface.
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