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TECHNIQUES FOR DYNAMIC STALL ANALYSIS
ANALYSIS OF DYNAMIC STALL EVENTS
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aircraft airfoil alloy analysis angle approach attitude band blade segments boundary layer Center characteristics compared comparisons configuration Continued correction couples degradation determined difference diffusion direction display distortion dynamic stall edge effect Entropy equal equation error Figure flap flight flow flow reversal flyover force frequency hover increasing indicated integration interval leading leading-edge mean measured methods NACA NASA noise normal number of blades observed obtained occur OOOO oscillation percent performance phase pilot pitching position preemphasis present pressure quantizers range recession reduced reference relative Report representative Research response roll rotor separation shown shows simulation smoke ſº Space speed stall standard static strake values vehicle vortex wing