This deforming method coupled with ale euler solver is applied to simulate unsteady transonic flow about oscillating airfoil ( 2 - d ) and oscillating rigid rectangular wing ( 3 - d ) . computational results are in good agreement with experimental data 本文將網(wǎng)格變形方法與數(shù)值解算器耦合起來(lái)求解了二維振動(dòng)翼型繞流和三維振動(dòng)矩形機(jī)翼繞流,計(jì)算結(jié)果與實(shí)驗(yàn)結(jié)果一致,證明本文的數(shù)值方法具有較高的準(zhǔn)確性。