Email this article Poincaré–Andronov–Hopf Bifurcation in Clicking Oscillations on the Compound Supporting and Control Surfaces of Aircraft
- Authors: Tleulinov M.K.1
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Affiliations:
- Kazan National Research Technical University
- Issue: Vol 45, No 8 (2019)
- Pages: 786-789
- Section: Article
- URL: https://bakhtiniada.ru/1063-7850/article/view/208394
- DOI: https://doi.org/10.1134/S1063785019080145
- ID: 208394
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Abstract
Oscillations of catastrophic changes of shape (clicking oscillations) of compound supporting and control surfaces interconnected in a statically indefinable manner are treated. The effect of the angle of attack on the nature of oscillations is investigated. The phase patterns of the control surface twist angle at different angles of attack are shown.
About the authors
M. K. Tleulinov
Kazan National Research Technical University
Author for correspondence.
Email: mktleulinov@kai.ru
Russian Federation, Kazan, Tatarstan, 420015
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