NASA NTRS · 19880008223
Fixed wing CCW aerodynamics with and without supplementary thrust deflection
Abstract
The concept of circulation control was successfully demonstrated in flight using an A-6 aircraft. Circulation control can provide an aircraft with STOL performance of heavy lift capability. For ship based Naval aircraft the lower takeoff and landing velocities result in reduced deck gear and wind over the deck requirements. Circulation control airfoils can be mechanically less complex and lightweight compared to multi-element high lift airfoils.
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Nichols, J. H., Harris, M. J.. 1987-05-01. Fixed wing CCW aerodynamics with and without supplementary thrust deflection. https://ntrs.nasa.gov/citations/19880008223
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