VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University62010.18287/2541-7533-2008-0-3(16)-114-118UnknownCalculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stageBaturinO. V.matveev.vn@ssau.ruMatveevV. N.matveev.vn@ssau.ruSamara State Aerospace University180920087311411804062014Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>The result of calculated study are stated and the changes of flow and losses structure in vane rows in transonic turbine stage by the tangential inclination of nozzle vanes have been justified in given article. Recommendations on the choice of bent vanes shape of the nozzle vane row have been suggested.</p>Nozzle bladeturbineeffectivenesspitchforceperipherysuction face of bladepanpressureСопловая лопаткатурбинаэффективностьнаклонсилапериферияспинкакорытцедавление