ALLEVIATION OF ROTOR BLADE DYNAMIC STALL VIA TRAILING EDGE FLAP FLOW CONTROL
41st, Aerospace sciences meeting ; 2003 ; Reno, NV
2003-01-01
ALL
Paper nos AIAA-2003-0001 to AIAA-2003-1359 with gaps
Conference paper
English
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Alleviation of airfoil dynamic stall moments via trailing-edge-flap flow control
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