摘要
在在接近音速的流动的弄弯的表面的正常吃惊导致一个超级坚定的边界价值问题。在吃惊后面的一个肿块减少机翼和还原剂的 drag 必要精力。在 contrary to 潜水艇的非牛顿的媒介铅的流动决定了边界起始的问题。为这些液体的精力平衡具有为化学工程的大兴趣。
The normal shock at a curved surface in transonic flow leads to a superdetermined boundary value problem. A bump behind the shock decreases the drag of the airfoil and reduces the necessary energy. Flows of non-Newtonian media lead in the contrary to subdetermined boundary initial problems. The energy balance for these fluids is of great interest for chemical engineering.
关键词
超音速流
震动
非牛顿介质
流体动力学
Transonic flow, Shock at a curved wall, Superdetermined problem, Non- Newtonian media, Subdeermined problem, Energy balance.
