LAMINAR-TURBULENT TRANSITION FOR ATTACHED AND SEPARATED FLOW
A major challenge in the design of turbomachinery components for aircraft gas turbine engines is high cycle fatigue failures due to flutter. Of particular concern is the subsonic/transonic stall flutter boundary which occurs at part speed near the stall line. At these operating conditions the incide...
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Format: | Others |
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UKnowledge
2010
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Online Access: | http://uknowledge.uky.edu/gradschool_diss/118 http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1122&context=gradschool_diss |