Active flow control bump design using hybrid Nash-game coupled to evolutionary algorithms

D Lee, J Periaux, L Gonzalez, K Srinivas… - Proceedings of the …, 2010 - eprints.qut.edu.au
In this paper, the optimal design of an active flow control device; Shock Control Bump (SCB)
on suction and pressure sides of transonic aerofoil to reduce transonic total drag is …

[PDF][PDF] ACTIVE FLOW CONTROL BUMP DESIGN USING HYBRID NASH-GAME COUPLED TO EVOLUTIONARY ALGORITHMS

DS Lee, J Periaux, LF Gonzalez… - Conference on …, 2010 - researchgate.net
Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic
total drag is investigated. Two optimisation test cases are conducted using different …

[PDF][PDF] ACTIVE FLOW CONTROL BUMP DESIGN USING HYBRID NASH-GAME COUPLED TO EVOLUTIONARY ALGORITHMS

DS Lee, J Periaux, LF Gonzalez, K Srinivas, E Onate - congress2.cimne.com
Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic
total drag is investigated. Two optimisation test cases are conducted using different …

[PDF][PDF] ACTIVE FLOW CONTROL BUMP DESIGN USING HYBRID NASH-GAME COUPLED TO EVOLUTIONARY ALGORITHMS

DS Lee, J Periaux, LF Gonzalez, K Srinivas… - … on Computational Fluid …, 2010 - academia.edu
Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic
total drag is investigated. Two optimisation test cases are conducted using different …

[PDF][PDF] ACTIVE FLOW CONTROL BUMP DESIGN USING HYBRID NASH-GAME COUPLED TO EVOLUTIONARY ALGORITHMS

DS Lee, J Periaux, LF Gonzalez, K Srinivas… - … on Computational Fluid …, 2010 - core.ac.uk
Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic
total drag is investigated. Two optimisation test cases are conducted using different …

[PDF][PDF] ACTIVE FLOW CONTROL BUMP DESIGN USING HYBRID NASH-GAME COUPLED TO EVOLUTIONARY ALGORITHMS

DS Lee, J Periaux, LF Gonzalez… - Conference on …, 2010 - researchgate.net
Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic
total drag is investigated. Two optimisation test cases are conducted using different …