Investigations on symmetric and asymmetric NACA airfoils with different thickness ratios flow and acoustic characteristics
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Date
2023-02
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Indian Institute of Technology (Indian School of Mines) Dhanbad
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Keywords
Aerodynamics, Symmetric NACA airfoils, asymmetric NACA airfoils, thickness ratios, laminar separation bubble, pressure coefficient, Ph.D, MECH, PH2400