Compressor Cascade - Globe Thesis

Keyword [Compressor Cascade] Result: 61 - 80 \| Page: 4 of 5
61.	Numerical Investigation Of Controlling Secondary Flow In High-speed Compressor Cascade Using Endwall Fences
62.	Influence Of Elliptic Tubercle Leading Edge Blade Modification In Linear Compressor Cascade
63.	Flow Control Mechanism Of Synthetic Jet In A Low-reaction Compressor Cascade
64.	Influence Of The Trailing Edge Serration On The Aerodynamic Performance Of A High Speed Compressor Cascade
65.	Numerical Investigation Of Boundary Layer Suction In A Highly-loaded Sectorial Compressor Cascade
66.	Influence On Performances Of High-load Rectangular Compressor Cascade With Boundary Layer Suction
67.	Application Study Of Fence In Static Flow Field Under The Condition Of Non-uniform Inlet
68.	Research On The Tip Vortex Structure And Unsteady Flow Control Of Compressor Cascade
69.	Numerical Study On Aerodynamic Performance Of Highly Loaded Compressors With Endwall Boundary Layer Suction
70.	Research On Thr Applicability Of Curved Blade In High Subsonic Compressor Cascade Design
71.	Application Study Of Co-Kriging Surrogate Model In Compressor Cascade Aerodynamic Optimization
72.	Investigation Of Corner Separation Control For Compressor Cascade Based On Vortex Generator
73.	Effect Of Serrated Trailing Edge On Aerodynamic Performance Of High-load Compressor Cascade
74.	Influence Of Bump On The Aerodynamic Performance Of Transonic Compressor Cascade
75.	Numerical Study Of Dimples On The Aerodynamic Performance Of A Transonic Rectangular Compressor Cascade
76.	Numerical Study On The Effect Of Boundary Layer Suction On A Transonic Sectorial Compressor Cascade
77.	Influence Of Tip Winglet Combined With Groove On The Tip Clearance Flow Of Compressor Stator
78.	Influence Of Bump Modeling Methods On The Aerodynamic Performance Of Transonic Compressor Cascade
79.	Numerical Study Of The Effect Of The Tip Cells On The Tip Clearance Flow Characteristics In A Compressor Cascade
80.	Numerical Study Of The Influence Of Spherical Dimple On The Aerodynamic Performance Of Transonic Sectorial Compressor Cascade
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