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이창훈(C. H. Lee),정성기(S. K. Jung),노국현(K. H. Rho),양영록(Y. R. Yang),명노신(R. S. Myong),조태환(T. H. Cho) 한국전산유체공학회 2010 한국전산유체공학회 학술대회논문집 Vol.2010 No.11
The concept of truncated airfoil sections has been suggested in order to extend the operational range of icing tunnels. With proper deflection of the small trailing-edge flap on the truncated airfoil the local pressure distribution may remain very close to that of the full-chord airfoil. The truncated flapped airfoil shape is studied by applying optimization methods. To verify the optimized truncated flapped airfoils, air flow and collection efficiency over the truncated airfoil are compared with the results of the full-scale airfoil by a computational method.