Particle Swarm Optimization of Suction and Blowing on Airfoils at Transonic Speeds
Autor: | Bedri Yagiz, Osama A. Kandil, Y. Volkan Pehlivanoglu, Oktay Baysal |
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Rok vydání: | 2010 |
Předmět: | |
Zdroj: | Journal of Aircraft. 47:1955-1965 |
ISSN: | 1533-3868 0021-8669 |
DOI: | 10.2514/1.c000233 |
Popis: | To improve the aerodynamic performance, the control applied to the transonic flow past an airfoil is optimized. The flow is simulated by solving the Navier–Stokes equations and a turbulence model. The control is applied using flow suction or blowing on the airfoil surface. The design variables are set to be the location and the angle of the suction/blowingport and themassflowcoefficient at this port. To validate the computationalmethodology, successful comparisons have beenmadewith available experimental data. The focus of the present study is on the application of a selected design optimization methodology. Therefore, the particle swarm optimization algorithm is also validated by comparing its results with those from a more traditional approach: that is, a gradient-based method with sequential quadratic programming. It is observed that the aerodynamic performance is increased by over 20% as a result of optimizing the location, angle, and mass flow coefficient of the suction and blowing control ports on the airfoil surface at transonic speeds. |
Databáze: | OpenAIRE |
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