boundary layer transition - Globe Thesis

Keyword [boundary layer transition] Result: 1 - 20 \| Page: 1 of 2
1.	Experimental Investigation Of Supersonic Boundary Layer And Shock Wave/Boundary Layer Interaction
2.	A Study Of Low-Reynolds-Number Performance Over A Two-Dimensional Airfoil For Micro-Air Vehilce
3.	Investigation Of Control Surface Hinge Moment Characteristic At Low Speed
4.	The Influence Of Root Fillet And Boundary Layer Transition On The Aerodynamic Performance Of Centrifugal Impeller
5.	Experimental Investigations Of Hypersonic Boundary Layer Transition On A Sharp Cone Based On The Method Of Wavelet Analysis
6.	Study On Wind Characteristics At Bridge Site In A Deep-Cutting Gorge By Wind Tunnel Test And CFD Method
7.	Direct Numerical Simulation Of Roughness-induced Transition In Hypersonic Boundary Layer
8.	Investigations Of Corner Separated Flow Loss Mechanism And Its Flow Control Techniques For Axial-compressors
9.	High-fidelity Aerodynamic Shape Optimization Method Of Aircraft Based On Computational Fluid Dynamics
10.	Research Of Engineering Method And Numerical Computation On Aerodynamic Heating Over Projectiles’ Head At High Speed
11.	Application Research Of Transonic Compressor Rotor By Large-Eddy Simulation
12.	Research On The Mechanism Of Boundary Layer Flow In Low Pressure Turbine Blade
13.	Study Of Shock Wave/Boundary Layer Interaction And Boundary Layer Transition Using High-order Numerical Scheme
14.	Experimental Investigation Of Transition Location Measurement And Control Based On A Variety Of Measurement Methods
15.	Research On Two-dimensional Forebody Boundary Layer Transition
16.	Synergistic Reduction Mechanism On Aerodynamic Drag And Noise Via Bionic Non-smooth Autobody
17.	Optimization Platform And Research On Compressor Cascade Flow
18.	Modification Of ?-Re_? Transition Model And Numerical Study Of Relevant Magnus Mechanism Of Rotating Body Of Revolution
19.	Experimental And Numerical Simulation Of Boundary Layer Transition Of Curved Surfaces
20.	Study On Fast Calculation Of Complex Shape Rocket Projectile Aerodynamic Heating Considering Transition Effect
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