A Hybrid Finite Difference and RBF-FD Simulation of Flow over a NACA  0012 Airfoil at Multiple Angles of Attack

Nikunja Bihari Barik

A Hybrid Finite Difference and RBF-FD Simulation of Flow over a NACA 0012 Airfoil at Multiple Angles of Attack

Authors

Nikunja Bihari Barik

Keywords:

Meshfree method, NACA 0012 airfoil problem, angles of attack, Streamline.

Abstract

An accurate hybrid mesh-based Finite Difference Method (FDM) and meshless Radial Basis Function-generated Finite Difference

References

Hirsch, C., Numerical Computation of Internal and External Flows, Computers & Fluids,

(1989), pp. 385–386.

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Published

2026-06-18

How to Cite

Nikunja Bihari Barik. (2026). A Hybrid Finite Difference and RBF-FD Simulation of Flow over a NACA 0012 Airfoil at Multiple Angles of Attack. Journal of Computational Analysis and Applications (JoCAAA), 35(6), 171–179. Retrieved from https://www.eudoxuspress.com/index.php/pub/article/view/5596