Investigation of relative geometric parameters influence on bypass engine mass

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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

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