Результаты аэродинамических исследований окружной неравномерности давлений за последней ступенью ЦНД паровой турбины

Abstract

Experimental data concerning the peripheral pressure nonuniformity behind the last stage of the low pressure turbine is given. The experiment was held on the air turbine at the changing of the operation mode and the size of exhaust manifold. The received results are represented by the function.