Numerical investigation on flow control effects of dynamic hump for turbine cascade at different Reynolds number and hump oscillating frequency
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DOI: 10.1016/j.ast.2019.05.070
Abstract: Abstract From takeoff to cruise, the operating Reynolds number (Re) of the low-pressure turbine (LPT) in an aero-engine decreases significantly, making the boundary layer near the aft portion of the blade surface susceptible to separation.… read more here.
Keywords: cascade; hump; hump oscillating; frequency ... See more keywords