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- W2371712184 abstract "This paper puts forward an optimization design approach for 2-D cascade based on niche genetic algorith-m.The approach designs the thicknessless wing initial bone line by using singularities method.Given determined most thic-kness, the airfoil can be obtained by thickening the known bone line according to the thickness distribution law of NACA-0012 aerodynamic airfoil,consequently the 2-D cascade can be achieved. Then, it searches the best bone line through minimizing the flow loss of the cascade surface boundary layer by using genetic algorithm.The computer program based on Boundary Element Method accomplishes the flow field analysis of known cascade. Assumed that the total loss has a direct proportion with the flow loss of the cascade surface boundary layer, the loss can be gained by calculating boundary layer using integral method. Applied the approach above said to the design of ZZ440 cascade,the result is proved to be effective and feasible." @default.
- W2371712184 created "2016-06-24" @default.
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- W2371712184 date "2002-01-01" @default.
- W2371712184 modified "2023-10-06" @default.
- W2371712184 title "APPLICATION OF GENETIC ALGORITHM IN OPTIMIZATION DESIGN FOR 2-D CASCADE BY USING SINGULARITIES METHOD" @default.
- W2371712184 hasPublicationYear "2002" @default.
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