Invention Application
WO1988009745A1 DIVERGENT TRAILING-EDGE AIRFOIL 审中-公开
潜水拖车边缘航空

DIVERGENT TRAILING-EDGE AIRFOIL
Abstract:
A special contour near the trailing edge (24) of an airfoil (20) which improves the airfoil effectiveness. The contour is a combination of a blunt airfoil base (28), a local region of high surface curvature, typically on the airfoil lower surface, and upper surface and lower surface trailing edge slopes that diverge from each other (30).
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