airfoil buffet boundary is an important aerodynamic parameter which is second only to the lift-drag ratio.
翼型抖振边界是仅次于升阻比的一项重要气动指标。
they also can expand the buffet boundary and decrease the buffet intensity. as a result, the large angle-of-attack flying quality can be significantly improved by utilization of maneuvering flaps.
它能控制气流分离和减小大迎角时的阻力,提高抖振边界和降低抖振强度,改善大迎角的飞行品质。
furthermore, the buffet boundary correlation for the jl-6 aircraft was analyzed using the data obtained from wind tunnel tests and the flight test data of the jl-6 aircraft.