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Question 2 (10 marks) (2022 Paper) Question 2a The Aerodynamic characteristic of a NACA0015 airfoil is simulated using a Potential Method. The Cp and Tw distributions are presented in Figure Q2(a)-1 and Q2(a)-2 of Appendix 1 respectively. Question 2a(i) Verify boundary layer transition occurrence by identifying the loc
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