The method of bypass engines turbocompressors structural-geometric parameters matching

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Abstract

The article describes the method of bypass engines turbocompressors structural-geometric parameters matching intended for use in the computer-aided thermogasdynamic design systems.

About the authors

I. N. Krupenich

Samara State Aerospace University

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

V. S. Kuzmichev

Samara State Aerospace University

Email: sadohina@ssau.ru
Russian Federation

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