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本文着重讨论如何用Head法来确定有局部激波的跨音速流动中的翼型分离点位置,并据此确定翼型抖振边界。文中还提出了如何修正Stratford方法,以便推广应用于同样目的。
This article focuses on how to determine the position of the airfoil separation point in a transonic flow with local shock using the Head method and determine the airfoil buffeting boundary. The article also proposed how to amend the Stratford method, in order to promote the use for the same purpose.