Gas-dynamic design of brake steps for axial microturbines


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Abstract

The calculation and research of gas-dynamic design of multistage axial microturbines with the limited frequency of rotation are given. The generalization of the results of this research as the recommendations by definition of number of brake steps and constructive-geometrical parameters of structures of working wheels of these steps is executed.

About the authors

N. F. Musatkin

Samara State Aerospace University

Author for correspondence.
Email: vest@ssau.ru
Russian Federation

V. M. Rad’ko

Samara State Aerospace University

Email: vest@ssau.ru
Russian Federation

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Copyright (c) 2019 VESTNIK of Samara University. Aerospace and Mechanical Engineering

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