Comparison and Analysis of Natural Laminar Flow Airfoil Shape Optimization Results at Transonic Regime with Bumps and Trailing Edge Devices Solved by Pareto Games and EAs

Author:

Chen Yongbin,Tang Zhili,Periaux Jacques

Publisher

Springer International Publishing

Reference10 articles.

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2. Chen, Y.B., Tang, Z.L., Sheng, J.D.: Multi objective optimization for natural laminar flow airfoil in transonic flow. Chin. J Phys 33(3), 283–296 (2016)

3. Tang, Z.L., Chen, Y.B., Zhang, L.H., Periaux, J.: Solving the two objective evolutionary shape optimization of a natural laminar airfoil and shock control Bump with Game Strategies. Arch. Computat. Meth. Eng. 26, 119–141 (2019)

4. Chen, Y.B., Tang, Z.L., Sheng, J.D.: Trailing edge device application to wave drag reduction in NLF airfoil multi-island design optimization. J. Nanjing Univ. Aeronaut. Astron. 50(4), 548–557 (2018)

5. Cebeci, T., Cousteix, J.: Modeling and Computation of Boundary Layer Flow: Laminar, Turbulent and Transitional Boundary Layers in Compressible Flows. Horizons Publishing, Long Beach (2003)

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