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Philadelphia, USA |
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* Scientific Article * Impact Factor 6.630 |
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Chemezov, D., et al.
Numerical simulation of aerodynamic characteristics of helicopter rotor blades. |
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Full Article: PDF
Scientific Object Identifier: http://s-o-i.org/1.1/TAS-07-123-26
DOI: https://dx.doi.org/10.15863/TAS.2023.07.123.26
Language: English
Citation: Chemezov, D., et al. (2023). Numerical simulation of aerodynamic characteristics of helicopter rotor blades. ISJ Theoretical & Applied Science, 07 (123), 234-237. Soi: http://s-o-i.org/1.1/TAS-07-123-26 Doi: https://dx.doi.org/10.15863/TAS.2023.07.123.26 |
Pages: 234-237
Published: 30.07.2023
Abstract: The results of helicopter flight simulation under conditions of the development of the rotor speed up to 300 rpm were presented in the article. Vector schemes of load distribution and air flow velocity along the length of the rotor blades were demonstrated. The results of numerical simulation of the deflection of the rotor blades were presented during takeoff and flight of the helicopter. The aerodynamic characteristics and the material stress of the rotor blades for one revolution around its axis were analyzed.
Key words: helicopter, rotor blade, lift force, degree.
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