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Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
Authors:A?E?Remizov  V?V?Vyatkov  Email author" target="_blank">V?A?LebedevEmail author
Institution:1.Rybinsk State Aviation Technical University,Rybinsk,Russia
Abstract:Methods to control flow have been considered in order to reduce end losses in blade rows of GTE gas turbines by means of measures taken at the design stage.
Keywords:
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