inlet distortion - Globe Thesis

Keyword [inlet distortion] Result: 1 - 20 \| Page: 1 of 2
1.	The Unsteady Mechanism And The Role Of Tip Clearance Flow In Distortion Induced Instability In An Axial Compressor
2.	Design And Aerodynamic Performance Study Of An S-shaped Inlet Of The UAV
3.	Research On Inlet Distortion's Effect On Aero-engine Using Parallel Compressor Model
4.	Investigation Of S-shaped Inlet Distortion Control And Its Impact On The Flow Field Of The Rear Transonic Fan-stage
5.	Investigations Of The Non-axisymmetric Flow Behaviors In Centrifual Compressor And The Effects Of The Inlet Distortion On The Internal Flow
6.	Research On Stability Control For Aero-Engine With Inlet Distortion
7.	The Effect Of Tip Injection On The Compressor Stability
8.	Research On Influences Of Inlet Distortion And Fuel InjectionPulse On Combustor Combustion Flow Field
9.	Investigation Of Internal Flow Field Characteristics Under Inlet Distortion In Dual Boost Compressor
10.	Investigation Of Performance Test And Flow Field Characteristics Under Bend Pipe Inlet Conditions In Centrifugal Compressor
11.	Numerical Study Of Stage Effects On Performance Of Centrifugal Compressors With Large Flow Coefficient
12.	Inlet Total Pressure Distortion Modeling And Stability Analysis Of High Bypass Ratio Turbofan Engine
13.	Investigation On The Mechanism Of Effects Of Rotating Inlet Distortion On Compressor Aerodynamic Stability
14.	Investigation Of Non-axisymmetric Flow Behaviors In Centrifugal Compressor Under Inlet Distortion
15.	Investigations On The Flow Characteristic And Forced Response Of Turbocharger In Pulsating And Distortion Inlet Conditions
16.	A Stall Warning Scheme For Axial Compressors With Inlet Distortion Via Deterministic Learning
17.	Aerodynamic Stability Assessment And Software Research Of High Bypass Ratio Turbofan Engine
18.	Investigations On Predicting Method Of Influence Of Inlet Flow Distortion On The Stability Of Variable Cycle Engine
19.	Study On The Application Of Unsymmetrical Impeller In Double-sided Centrifugal Compressor And The Uniformity Of Circumferential Flow Field
20.	Research On Boundary Layer Suction Mechanism And Influence Effect Of Axial Flow Compressor
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