Investigation of relative geometric parameters influence on bypass engine mass

Abstract

Influence of relative diameters of bypass engine turbocompressor on its mass is described.

About the authors

V. S. Kuzmichev

Samara State Aerospace University

Author for correspondence.
Email: kuzm@ssau.ru

Doctor of Science

Professor at Aircraft Engine Theory Department

Russian Federation

I. N. Krupenich

Samara State Aerospace University

Email: kru@ssau.ru

Candidate of Science

Associate professor at Aircraft Engine Theory Department

Russian Federation

V. V. Kulagin

Samara State Aerospace University

Email: kulvv@ssau.ru

Candidate of Science

Professor at Aircraft Engine Theory Department

Russian Federation

E. S. Miheeva

Samara State Aerospace University

Email: kulvv@ssau.ru
Student Russian Federation

A. A. Nikolaev

Samara State Aerospace University

Email: kulvv@ssau.ru
Student Russian Federation

References

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