Airfoil buffetboundary 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。
2
Furthermore, the buffetboundary 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.
利用风洞试验和飞行试验得到的数据进行了JL - 6飞机抖振边界相关性分析。
3
They also can expand the buffetboundary and decrease the buffet intensity. As a result, the large angle-of-attack flying quality can be significantly improved by utilization of maneuvering flaps.