NASA NTRS · 19920000037
Stall-Departure-Resistance Enhancer
Abstract
Stall-departure-resistance enhancer imposes lesser drag penalty than nortex generators of older types. Increases lift by as much as 30 percent at angles of attack otherwise in poststall region. Device is flat plate wedge with 60 degree sweep angle and attached so it protrudes from leading edge of wing. Tip is sharp point, and edges made thin and sharp to induce good vortical flow. Applications include those intended to increase safety for broad range of aircraft, including trainers, fighters, general-aviation aircraft, and commercial transport aircraft. Nonaerospace applications where flow stall is problem under certain conditions, such as in control of separation in flow diffusers. Other applications in fluid machinery and fluid flow.
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Ross, Holly M., Johnson, Joseph L., Jr., Yip, Long P., Stough, H. Paul, III. 1992-01-01. Stall-Departure-Resistance Enhancer. https://ntrs.nasa.gov/citations/19920000037
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