Active flow control of ship deck coupled flow field based on jet flow

被引:0
|
作者
Zhao J. [1 ]
Han D. [1 ]
Yu L. [2 ]
机构
[1] National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] School of Aeronautics and Astronautics, Sun Yat-Sen University, Guangzhou
关键词
active flow control; flow field of deck; jet flow; numerical simulation; shipboard helicopter;
D O I
10.11918/202201050
中图分类号
学科分类号
摘要
The rapid development and extensive application of ships highlight the vital role of the analysis and control of ship deck flow field. To improve the flow field of ship deck, a novel active flow control method based on jet is proposed, and by taking the position of helicopter rotor disk as an example, the effect of different jet device parameters on the optimization of helicopter rotor disk flow field is analyzed. First, the numerical simulation model of the flow field of the ship deck was established to examine the influence of active flow control on the ship deck flow field based on the Navier-Stokes equation. Then, the k-ε turbulence model was chosen and the effectiveness of the method was validated. Finally, the streamline and velocity distribution of ship deck flow field with jet device were simulated. Combined with the influence of flow field information on rotor force, the flow control effect of jet device on ship deck flow field was compared and analyzed. The results show that the addition of upper jet can reduce the influence range of reflux zone in the deck flow field and the velocity gradient of rotor disk flow field accordingly. The reduction of the velocity gradient of the rotor disk flow field tends to effectively reduce the aerodynamic variation and the response of the rotor. Adding jet devices under different inflow angles may reduce the response and improve the safety of the helicopter by controlling the deck flow field. As the jet velocity exerts a significant influence on the flow field control effect, the optimal jet velocity should be selected with reference to the installation position of the jet device to achieve better control effect. © 2023 Harbin Institute of Technology. All rights reserved.
引用
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页码:26 / 34
页数:8
相关论文
共 20 条
  • [1] KELLER J A, SMITH E C., An experimental and theoretical correlation of helicopter rotor blade droop impacts, Journal of Aircraft, 36, 2, (1999)
  • [2] GAONKAR G H., On modeling and simulation of airwake and airwake-downwash turbulence for helicopter shipboard operations, Proceedings of the 69th American Helicopter Society International Annual Forum, (2013)
  • [3] HAN Dong, YU Lei, BARAKOS G N., Transient aeroelastic response control of shipboard rotors during engagements by gurney flaps, Journal of Aircraft, 56, 2, (2019)
  • [4] BROWNELL C J, LUZNIK L, SNYDER M R, Et al., Velocity measurements in a ship airwake with crosswind, Proceedings of the 42nd Fluid Dynamics Conference and Exhibit, (2012)
  • [5] RAJAGOPALAN G, SCHALLER D, WADCOCK A J, Et al., Experimental and computational simulation of a model ship in a wind tunnel, Proceedings of the 43rd Aerospace Science Meeting and Exhibit, (2005)
  • [6] ROSENFELD N C, KIMMEL K R, SYDNEY A J., Investigation of ship topside modeling practices for wind tunnel experiments, Proceedings of the 53rd Aerospace Science Meeting, (2015)
  • [7] POLSKY S A, BRUNER C W S., Time-accurate computational simulations of an LHA ship airwake, Proceedings of the 18th Applied Aerodynamics Conference, (2000)
  • [8] SHARMA A, LONG L N., Airwake simulations on an LPD 17 ship, Proceedings of the 15th Computational Fluid Dynamics Conference, (2001)
  • [9] FORREST J S, HODGE S J, OWEN I, Et al., An investigation of ship airwake phenomena using time-accurate CFD and piloted helicopter flight simulation, Proceedings of the 34th European Rotorcraft Forum, (2008)
  • [10] CZERWIEC R M, POLSKY S A., LHA airwake wind tunnel and CFD comparison with and without bow flap, Proceedings of the 22nd Applied Aerodynamics Conference and Exhibit, (2004)