Алгоритм оптимального проектирования сопловой решетки осевой турбины с помощью аэродинамической обратной задачи

Abstract

The algorithm of optimal design turbine cascade with assistance aerodynamic inverse problem, which to take account limitation on strength is introduce. The new profile of stator cascade which has local wavy contours and the coefficient of total losses is much lower, than at an initial cascade of atlas profile is designed.