Air cooling of a turbine guide vane for a stationary gas-turbine plant (GTP) with a high gas pressure

A guide vane for a proposed stationary GTP is calculated with _r=80, 100, and 126 and T_g^*=1673°K. The unsuitability of the convective blade cooling used up to now is noted.Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 34, No. 5, pp. 897–902, May, 1978.