Experimental Study of Aerodynamics Performance of NACA4418 Airfoil with Fencing

Author:

Balaji G.,Snehit Chebrolu Sai,Eswar Alapati Bipin Sai,Singha Debayan,Mitra Mainak,Nagarajan S.,Santhosh Kumar G.

Publisher

Springer Nature Switzerland

Reference13 articles.

1. Alam, M., Kara, K., & Alexander, A. (2022). Reduction of spanwise flow over a swept wing using an air curtain produced by rectangular slot. In AIAA AVIATION 2022 Forum.

2. Balaji, G., Raj, M. S., Aswin, S. K. S., Kabilan, K., & Navinkumar, B. (2022a). Effect of angle of attack on pressure distribution of NACA5520 airfoil blade. International Journal of Vehicle Structures & Systems, 14(1), 93–98.

3. Balaji, G., Gupta, S., Manikpuri, G. K., Sureshkumar, S., Sathish, S., & Madhanraj, V. (2022b). Numerical investigation of aerodynamic performance of leading edge tubercle airfoil at low Reynolds number. Materials Today: Proceedings, 68, 1455–1465.

4. Cerón-Muñoz, H. D., et al. (2016). Experimental analyses of droop, wingtips and fences on a BWB model. In Proceedings of the 30th Congress of the International Council of the Aeronautical Sciences (ICAS 2016), Daejeon, Korea.

5. Demoret, A. C., Walker, M. M., & Reeder, M. F. (2020). The effect of passive boundary-layer fences on delta wing performance at low Reynolds number. In AIAA Scitech 2020 Forum.

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