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Extra info for Proceedings of the International Conference on Experimental Fluid Mechanics (2nd)
The hysteric behavior of the unsteady loads is a result of the lag in vortex breakdown due to the models motion. Although we have made much progress in understanding the flow structure of leading-edge vortices before and after breakdown, a comprehensive theory for breakdown still is unavailable. On the other hand, the experimental studies conducted during the past decade have provided details of the flow that may allow for the development of a new theoretical model or an improvement of one of the existing theories.
N. ; ................... i .. .. .. .. . • . .. -.. : .............. .... ...... S.............................. -.. ;............... S............. . I ..... 10 20 30 . 4.. :.. 4 .. ............ p... " ' •' ''L"• ' '. I I l 40 "- '" -' " ........... 50 60 70 80 90 100 AGE(Years) Figure 1. Variation of Formation number with age (a --• normal patients. • -* DCM) The mean value of 4 for the formation number appears to indicated the existence of a universal time scale that describes left ventricle flows during diastole.
As the wing pitches down, the leading-edge vortex system reforms with breakdown near the apex. Breakdown then moves aft as the angle of attack continues to decrease. These data illustrate the lags that develop for the unsteady case. For the upward motion, there is a lag in the development of the vortex core and the upstream progression of vortex breakdown. For the downward motion there is a lag in reformation of the vortex system (from fully separated flow conditions) and thus in the downstream progression of vortex breakdown.