Wang recalls that the US Air Force Academy and the University of Colorado in Boulder this year experimented on a wing designed to undergo torsional limit cycle oscillation, also known as stall flutter. These flow control experiments and matching simulations suggest that such flutter can be significantly reduced by modifying the flow structure with a jet of air injected through a small slot near the leading edge. Here, she also looks at other flow-control technologies.
Flow-control technologies move out of labs
Aerospace America ; 53 , 11
2015
Article (Journal)
English
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