TY - GEN
T1 - Estimation of Induced Velocity of Helicopter Rotor Blade for Controlling and Stability
AU - Tikle, Aayush Manish
AU - Yadav, Manish Varun
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - This paper presents an analytical and simulated investigation of the helicopter rotor blade employing the NACA 0012 airfoil. The simulations are conducted using the CFD ++ software. A crucial parameter for stress and pressure analysis of underlying structures is the induced velocity resulting from the downwash of the helicopter rotor. This induced velocity is intricately linked with the vertical climb velocity observed during the helicopter's ascent phase. The combination of induced velocity and vertical climb velocity contributes to the pressure distribution on objects within the downwash's sphere of influence. The process involves the utilization of Catia V5, SpaceClaim 22R1, MIME 8.1, CFD ++, and EXCEL software tools for tasks such as 3D modeling, geometry refinement, mesh generation, pre and post-processing, analysis, and visualization. The primary objective of this paper is to assess the induced velocity, pressure implications, and the flow-field characteristics within the proximate vicinity of the modeled helicopter rotor.
AB - This paper presents an analytical and simulated investigation of the helicopter rotor blade employing the NACA 0012 airfoil. The simulations are conducted using the CFD ++ software. A crucial parameter for stress and pressure analysis of underlying structures is the induced velocity resulting from the downwash of the helicopter rotor. This induced velocity is intricately linked with the vertical climb velocity observed during the helicopter's ascent phase. The combination of induced velocity and vertical climb velocity contributes to the pressure distribution on objects within the downwash's sphere of influence. The process involves the utilization of Catia V5, SpaceClaim 22R1, MIME 8.1, CFD ++, and EXCEL software tools for tasks such as 3D modeling, geometry refinement, mesh generation, pre and post-processing, analysis, and visualization. The primary objective of this paper is to assess the induced velocity, pressure implications, and the flow-field characteristics within the proximate vicinity of the modeled helicopter rotor.
UR - https://www.scopus.com/pages/publications/85195119631
UR - https://www.scopus.com/pages/publications/85195119631#tab=citedBy
U2 - 10.1109/TEMSCON-ASPAC59527.2023.10531530
DO - 10.1109/TEMSCON-ASPAC59527.2023.10531530
M3 - Conference contribution
AN - SCOPUS:85195119631
T3 - Proceedings of 2023 IEEE Technology and Engineering Management Conference - Asia Pacific, TEMSCON-ASPAC 2023
BT - Proceedings of 2023 IEEE Technology and Engineering Management Conference - Asia Pacific, TEMSCON-ASPAC 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2023 IEEE Technology and Engineering Management Conference - Asia Pacific, TEMSCON-ASPAC 2023
Y2 - 15 December 2023 through 16 December 2023
ER -