Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»

Abstract

Main underlying principles of the CAE-system «ASTRA» are 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

A. Yu. Tkachenko

Samara State Aerospace University

Email: tau@ssau.ru

Candidate of Science

Associate professor at Aircraft Engine Theory Department

Russian Federation

V. N. Rybakov

Samara State Aerospace University

Email: rybakov@ssau.ru

Post-graduate Student 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

References

  1. Кузьмичев, В.С. Моделирование полета летательного аппарата в задачах оптимизации параметров рабочего процесса газотурбинных двигателей [Текст] / В.С. Кузьмичев, А.Ю. Ткаченко, В.Н. Рыбаков – Известия Самарского научного центра Российской академии наук. – 2012. – т.14, №2(2). – С. 491-494.

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