Reduction of circumferential variation in the final stage of IPC

Cover Page

Cite item

Full Text

Abstract

Circumferential variation of the flow in final stage rotor wheel, caused by the support racks at the exit of the IPC, is evaluated by means of intermediate pressure of compressor of workflow 3D model. The methods of reducing the circumferential variation of flow by changing final stage’s guide vanes angles.

About the authors

G. M. Popov

Samara State Aerospace University

Author for correspondence.
Email: grishatty@mail.ru

Engineer of the Engine Theory Department

Russian Federation

A. C. Mamedov

Samara State Aerospace University

Email: grishatty@mail.ru

Student

Russian Federation

Y. D. Smirnova

Samara State Aerospace University

Email: pirajock@ya.ru

Student

Russian Federation

References

  1. Кулагин, В.В. Теория, расчёт и проектирование авиационных двигателей и энергетических установок [Текст]: учебное пособие / В.В. Кулагин. - М.: Машиностроение, 2002. - 616 с.

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies