AIRFOIL DESIGN OPTIMIZATION USING MULTI FIDELITY AT LOW REYNOLDS NUMBER FOR FIXED WING UAV
A methodology is given to choose an airfoil for a fixed wing UAV, and evaluate based on the mission constraints, and to efficiently optimize the airfoil by using multi-fidelity software such as XFLR5 and ANSYS FLUENT. The analysis solvers are validated for the wind tunnel test data of E387 and CAL2463m airfoil. Then, t...
Preety Kumari, Ashok Kuppusamy, Arnob Das Rudra
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