Email this article Investigation of Modeling Possibility for Lagging of a Helicopter Operating in Transient Flight Regimes
- Authors: Girfanov A.M.1, Ledyankina O.A.1, Gimadiev R.S.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- Kazan State Power Engineering University
- Issue: Vol 62, No 4 (2019)
- Pages: 719-721
- Section: Technical Notes
- URL: https://journals.rcsi.science/1068-7998/article/view/231215
- DOI: https://doi.org/10.3103/S1068799819040263
- ID: 231215
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Abstract
An invitational method is proposed for modeling transient loading processes of a helicopter during a flight. Formulas are presented, which allow performing imitation of lagging. An example of numerical modeling for a transient flight regime is presented.
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About the authors
A. M. Girfanov
Tupolev Kazan National Research Technical University
Email: led_o@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
O. A. Ledyankina
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: led_o@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
R. Sh. Gimadiev
Kazan State Power Engineering University
Email: led_o@mail.ru
Russian Federation, ul. Krasnosel’skaya 51, Kazan, 420066 Tatarstan
