Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method
This paper is dedicated to the numerical modeling of the aerodynamic characteristics of the full-scale coaxial main rotor. The modes of forward flight in the range of values V = 30−60 m∙s–1 (108−216 km∙h–1) have been under consideration. The simulation has been performed with the usage of two comput...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2022-03-01
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| Series: | Journal of Aerospace Technology and Management |
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| Online Access: | https://www.scielo.br/j/jatm/a/W33GmRXFxbQLGgxDV3CvM9m/?format=pdf&lang=en |
| _version_ | 1828326827561582592 |
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| author | Sergey Gennadievich Konstantinov Yuri Mikhailovich Ignatkin Pavel Viacheslavovich Makeev Alexander Ivanovich Shomov Sergey Olegovich Nikitin |
| author_facet | Sergey Gennadievich Konstantinov Yuri Mikhailovich Ignatkin Pavel Viacheslavovich Makeev Alexander Ivanovich Shomov Sergey Olegovich Nikitin |
| author_sort | Sergey Gennadievich Konstantinov |
| collection | DOAJ |
| description | This paper is dedicated to the numerical modeling of the aerodynamic characteristics of the full-scale coaxial main rotor. The modes of forward flight in the range of values V = 30−60 m∙s–1 (108−216 km∙h–1) have been under consideration. The simulation has been performed with the usage of two computational fluid dynamics (CFD) approaches: the free wake model (FWM) developed by the authors and the unsteady Reynolds-averaged Navier–Stokes (URANS) equations method based on the Ansys Fluent software. The coefficients of rotor thrust and torque, vortex wake shapes and induced velocity fields have been obtained and analyzed. The FWM and the URANS modeling data match satisfactorily. The FWM demonstrates a significant advantage in computing time and resources costs with sufficient accuracy in resulting rotor’s basic aerodynamic
characteristics. That’s why it seems appropriate to use the FWM for preliminary simulations, taking into account before using the high time and resource intensive the URANS method for comprehensive investigation of coaxial rotor aerodynamics at
forward flight modes.
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| first_indexed | 2024-04-13T19:45:56Z |
| format | Article |
| id | doaj.art-0156ea84f35f4804b22d9566119aae19 |
| institution | Directory Open Access Journal |
| issn | 1984-9648 2175-9146 |
| language | English |
| last_indexed | 2024-04-13T19:45:56Z |
| publishDate | 2022-03-01 |
| publisher | Instituto de Aeronáutica e Espaço (IAE) |
| record_format | Article |
| series | Journal of Aerospace Technology and Management |
| spelling | doaj.art-0156ea84f35f4804b22d9566119aae192022-12-22T02:32:44ZengInstituto de Aeronáutica e Espaço (IAE)Journal of Aerospace Technology and Management1984-96482175-91462022-03-01141e0822e0822https://doi.org/10.1590/jatm.v14.1250Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes MethodSergey Gennadievich Konstantinov0Yuri Mikhailovich Ignatkin1Pavel Viacheslavovich Makeev2Alexander Ivanovich Shomov3Sergey Olegovich Nikitin4Moscow Aviation Institute – National Research University – Aeronautical Engineering – Moscow – Russian Federation.Moscow Aviation Institute – National Research University – Aeronautical Engineering – Moscow – Russian Federation.Moscow Aviation Institute – National Research University – Aeronautical Engineering – Moscow – Russian Federation.Moscow Aviation Institute – National Research University – Aeronautical Engineering – Moscow – Russian Federation.Moscow Aviation Institute – National Research University – Aeronautical Engineering – Moscow – Russian Federation.This paper is dedicated to the numerical modeling of the aerodynamic characteristics of the full-scale coaxial main rotor. The modes of forward flight in the range of values V = 30−60 m∙s–1 (108−216 km∙h–1) have been under consideration. The simulation has been performed with the usage of two computational fluid dynamics (CFD) approaches: the free wake model (FWM) developed by the authors and the unsteady Reynolds-averaged Navier–Stokes (URANS) equations method based on the Ansys Fluent software. The coefficients of rotor thrust and torque, vortex wake shapes and induced velocity fields have been obtained and analyzed. The FWM and the URANS modeling data match satisfactorily. The FWM demonstrates a significant advantage in computing time and resources costs with sufficient accuracy in resulting rotor’s basic aerodynamic characteristics. That’s why it seems appropriate to use the FWM for preliminary simulations, taking into account before using the high time and resource intensive the URANS method for comprehensive investigation of coaxial rotor aerodynamics at forward flight modes. https://www.scielo.br/j/jatm/a/W33GmRXFxbQLGgxDV3CvM9m/?format=pdf&lang=encoaxial main rotorforward flightcfduransfree wake model |
| spellingShingle | Sergey Gennadievich Konstantinov Yuri Mikhailovich Ignatkin Pavel Viacheslavovich Makeev Alexander Ivanovich Shomov Sergey Olegovich Nikitin Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method Journal of Aerospace Technology and Management coaxial main rotor forward flight cfd urans free wake model |
| title | Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method |
| title_full | Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method |
| title_fullStr | Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method |
| title_full_unstemmed | Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method |
| title_short | Comparative Study of Coaxial Main Rotor Aerodynamics at Forward Flight Based on Free Wake Model and Unsteady ReynoldsAveraged Navier–Stokes Method |
| title_sort | comparative study of coaxial main rotor aerodynamics at forward flight based on free wake model and unsteady reynoldsaveraged navier stokes method |
| topic | coaxial main rotor forward flight cfd urans free wake model |
| url | https://www.scielo.br/j/jatm/a/W33GmRXFxbQLGgxDV3CvM9m/?format=pdf&lang=en |
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