Abstract
*† This paper focuses on enhanced airplane high-lift performance utilizing Active Flow Control (AFC). A Computational Fluid Dynamics process has been developed for the simulation of AFC interactive flows. The analysis tool has been validated with experimental data and it has been extensively used to gain insight into interactive flows which are subject to various modes of actuation. The computational method has been used for a methodical buildup of distributed flow control systems with substantial gains in aerodynamic efficiency. The versatility of the distributed active flow control offers high payoff for practical airframe integration of high lift systems.
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