CFD Analysis of Counter-Rotating Vane-Type Wing Vortex Generator for Regional Aircraft
DOI:
https://doi.org/10.37934/cfdl.16.11.116Keywords:
Wing Vortex Generator, Numerical Simulation, Stall, CFDAbstract
Vortex generator is a component that has a significant impact on aircraft performance. The function of the vortex generator is to create vortices that can optimize the aerodynamic performance of aircraft wings by avoiding air flow separation and increasing lift at high angle of attack. Vortex generator can provide increased lift during take-off and landing due to the increased wing angle of attack. Although the use of vortex generator can be carried out using an experimental approach, a computational fluid dynamic approach to determine the influence of geometric parameters and placement of the vortex generator needs to be carried out. The aim of this research is to determine the effect of parameters like placement on the wing chord, height of the boundary layer, length, shape, angle of incidence and distance between pairs on the lift and drag. The model used as a computational fluid dynamic calculation model is the Spalart Allmaras transient model. As a result, vortex generator does not always have a good effect on aerodynamics. All configurations have a negative influence on the lift and drag values, but the flow separation phenomenon can be reduced significantly. Of all the configurations, the best configuration is obtained by exhibiting an ogive shape, positioned at 13.8% of the chord length, set at a 13o angle of incidence. The vortex generator should have a height closely matching the boundary layer, with a length 6.5 times the height and a pair spacing of 6.7 times the height
Downloads
References
Babikian, Raffi, Stephen P. Lukachko, and Ian A. Waitz. "The historical fuel efficiency characteristics of regional aircraft from technological, operational, and cost perspectives." Journal of Air Transport Management 8, no. 6 (2002): 389-400. https://doi.org/10.1016/S0969-6997(02)00020-0
Merryisha, Samuel, and Parvathy Rajendran. "Experimental and CFD analysis of surface modifiers on aircraft wing: A review." CFD Letters 11, no. 10 (2019): 46-56.
Forster, K. J., and T. R. White. "Numerical investigation into vortex generators on heavily cambered wings." AIAA journal 52, no. 5 (2014): 1059-1071. https://doi.org/10.2514/1.J052529
J. Meyer, P. Okfen, and C. Bil, “Optimisation of Vortex Generators for Stall Speed Reduction,” 2021.
Reichert, B. A., and B. J. Wendt. "Improving curved subsonic diffuser performance with vortex generators." AIAA journal 34, no. 1 (1996): 65-72. https://doi.org/10.2514/3.13022
Lee, Sang, and Eric Loth. "Supersonic boundary-layer interactions with various micro-vortex generator geometries." The Aeronautical Journal 113, no. 1149 (2009): 683-697. https://doi.org/10.1017/S0001924000003353
Koike, Masaru, Tsunehisa Nagayoshi, and Naoki Hamamoto. "Research on aerodynamic drag reduction by vortex generators." Mitsubishi motors technical review 16 (2004): 11-16.
Agarwal, Shubham, and Priyank Kumar. "Numerical investigation of flow field and effect of varying vortex generator location on wing performance." American Journal of Fluid Dynamics 6, no. 1 (2016): 11-19.
Huang, Jingbo, Song Fu, Zhixiang Xiao, and Miao Zhang. "Study of separation control of vortex generators on transonic wings." Journal of Fluid Science and Technology 6, no. 1 (2011): 85-97. https://doi.org/10.1299/jfst.6.85
R. Srinath and D. Sahana, “Energization of Boundary Layer Over Wing Surface By Vortex Generators,” 2017.
Namura, Nobuo, Koji Shimoyama, Shigeru Obayashi, Yasushi Ito, Shunsuke Koike, and Kazuyuki Nakakita. "Multipoint design optimization of vortex generators on transonic swept wings." Journal of Aircraft 56, no. 4 (2019): 1291-1302. https://doi.org/10.2514/1.C035148
Ito, Yasushi, Kazuomi Yamamoto, Kazuhiro Kusunose, Shunsuke Koike, Kazuyuki Nakakita, Mitsuhiro Murayama, and Kentaro Tanaka. "Effect of vortex generators on transonic swept wings." Journal of Aircraft 53, no. 6 (2016): 1890-1904. https://doi.org/10.2514/1.C033737
Kuwik, Brett, Christopher Tabacjar, and Seong-jin Lee. "CFD investigation of vortex generator additions to the general atomics MQ-9 reaper." In 2018 AIAA Aerospace Sciences Meeting, p. 1009. 2018. https://doi.org/10.2514/6.2018-1009
Agarwal, Shubham, and Priyank Kumar. "Numerical investigation of flow field and effect of varying vortex generator location on wing performance." American Journal of Fluid Dynamics 6, no. 1 (2016): 11-19.
Zhen, Tan Kar, Muhammed Zubair, and Kamarul Arifin Ahmad. "Experimental and numerical investigation of the effects of passive vortex generators on Aludra UAV performance." Chinese Journal of Aeronautics 24, no. 5 (2011): 577-583. https://doi.org/10.1016/S1000-9361(11)60067-8
Thornburg, Hugh. "Overview of the PETTT Workshop on Mesh Quality/Resolution, Practice, Current Research, and Future Directions." In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, p. 606. 2012. https://doi.org/10.2514/6.2012-606
Bueno-Orovio, Alfonso, Carlos Castro, Francisco Palacios, and Enrique Zuazua. "Continuous adjoint approach for the Spalart-Allmaras model in aerodynamic optimization." AIAA journal 50, no. 3 (2012): 631-646. https://doi.org/10.2514/1.J051307
Acharya, S., B. R. Baliga, Kailash Karki, J. Y. Murthy, C. Prakash, and Surya Pratap Vanka. "Pressure-based finite-volume methods in computational fluid dynamics." (2007): 407-424. https://doi.org/10.1115/1.2716419
Latimer, B. R., and A. Pollard. "Comparison of pressure-velocity coupling solution algorithms." Numerical Heat Transfer 8, no. 6 (1985): 635-652. https://doi.org/10.1080/01495728508961876
De Rango, S., and D. W. Zingg. "Higher-order spatial discretization for turbulent aerodynamic computations." AIAA journal 39, no. 7 (2001): 1296-1304. https://doi.org/10.2514/2.1472
Downloads
Published
How to Cite
Issue
Section
