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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2022
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Article
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Fig 24
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Research Article
Trailing Edge Flap Effects on Dynamic Stall Vortex and Unsteady Aerodynamic Forces on a Pitching Airfoil
Figure 24
Schematic of airfoil shapes for different relative chord lengths of the TEF at the deflection angle of -20 deg.