supersonic airfoil

基本解釋

The approach can unify the subsonic, transonic and supersonic inverse problems and avoid the direct simulation of the unsteady wake of oscillating airfoil.
提出在映象坐標(biāo)下求解二維非定常歐拉方程獲取二維振蕩機(jī)翼的氣動(dòng)反命題解，給出了非定常氣動(dòng)反問題的邊界條件和求解方法。
Based on the piston theory of supersonic flow, the second lagrange equation is used to set up the dynamic equations of an airfoil with store in the supersonic or hypersonic flow.
基于超音速氣動(dòng)力活塞理論，采用第二類拉格朗日方程建立了帶外掛二元翼系統(tǒng)在超音速和超高音速氣流作用下的動(dòng)力學(xué)方程。