transonic equation信息详情
跨音速方程
equation───n.方程式,等式;相等;[化学]反应式
generative equation───生成方程
integral equation───[数]积分方程;积分方程(式)
cubic equation───[数]三次方程
fresnel equation───菲涅耳方程
equation editor───公式编辑器
interpolation equation───插值方程
adjoint equation───[数]伴随方程
regression equation───[数]回归方程;回归方程式
transonic flow field around NACA 0012 airfoil is calculated by finite element method from pressure minimum integration, full potential equation being used.───有限元法计算了NACA 0012翼型的跨音速流场。出发方程为全速位方程。
By numerically solving the inviscid, small disturbance equation in steady transonic regime, with boundary conditions on solid or porous airfoils, the corresponding pressure distribution is obtained.───通过数值求解定常跨音速流的无粘、小扰动方程,根据实心翼型或多孔翼型的边界条件,获得了相应的压力分布。
In this paper, a method for the transonic shock-free airfoil design, based on the full potential equation, using "fictitious gas" assumption, is presented.───本文采用全位势方程,在超音速区采用虚拟气体假设,给出了跨音速无激波翼型设计的一种方法。
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