Turbine Blade Tip Leakage Flow Control by Partial Squealer Tip and Plasma Actuators (AIAA2006-0020)
44th, 44th AIAA aerospace sciences meeting: a collection of technical papers; VOL 1 ; 2006 ; Reno, NV
01.01.2006
18 pages
Vol 1 of 24
Aufsatz (Konferenz)
Englisch
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Effect of Squealer Geometry Arrangements on Tip Leakage Flow and Heat Transfer for Turbine Blade
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|Squealer Tip Leakage Flow Characteristics in Transonic Condition
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