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Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»
- Authors: Kuzmichev V.S.1, Tkachenko A.Y.1, Rybakov V.N.1, Krupenich I.N.1, Kulagin V.V.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 11, No 5-1 (2012): Special Issue
- Pages: 160-164
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/1859
- DOI: https://doi.org/10.18287/2541-7533-2012-0-5-1(36)-160-164
- ID: 1859
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Abstract
Main underlying principles of the CAE-system «ASTRA» are described.
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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 FederationA. Yu. Tkachenko
Samara State Aerospace University
Email: tau@ssau.ru
Candidate of Science
Associate professor at Aircraft Engine Theory Department
Russian FederationV. N. Rybakov
Samara State Aerospace University
Email: rybakov@ssau.ru
Post-graduate Student at Aircraft Engine Theory Department
Russian FederationI. N. Krupenich
Samara State Aerospace University
Email: kru@ssau.ru
Candidate of Science
Associate professor at Aircraft Engine Theory Department
Russian FederationV. V. Kulagin
Samara State Aerospace University
Email: kulvv@ssau.ru
Candidate of Science
Professor at Aircraft Engine Theory Department
Russian FederationReferences
- 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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