Method of gas turbine engine control program and law optimization with accordance to efficiency parameters of aircraft

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Abstract

The article describes the method of gas turbine engine control program optimization with accordance to efficiency parameters of aircraft.

About the authors

V. S. Kuzmichev

Samara State Aerospace University

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

A. Y. Tkachenko

Samara State Aerospace University

Email: sadohina@ssau.ru
Russian Federation

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