hypersonic - Globe Thesis

Keyword [hypersonic] Result: 181 - 200 \| Page: 10 of 10
181.	Experiment Investigation On The Hypersonic Crossflow Instability Over The Swept Flat Plates And The Cone
182.	Numerical Analysis Of Magnetofluiddynamic Control On The Hypersonic Inlet Flow
183.	Numerical Study On Heat And Drag Reduction Of Transpiration With Chemical Nonequilibrium Flow Past A Blunt Body
184.	Shock Interactions In Hypersonic Internal Conical Flow
185.	Theoretical And Numerical Investigations On Transpiration Cooling Of Hypersonic Vehicles
186.	Research On Variational Optical Flow Particle Image Velocimetry In Hypersonic Flows
187.	Stability Analysis And Transition Control In Hypersonic Streamwise Vortices Over A Yawed Cone
188.	Study On Transition In A Hypersonic Swept Blunt Plate Boundary Layer
189.	Research On Non-contact Optical Measurement Technology Of Flow Field
190.	Research On Electromagnetic Scattering Characteristics And Feature Recognition Of Hypersonic Vehicles
191.	Study On Drag And Heat Reduction Mechanism And Flow Instability Characreristics Of Hypersonic Countreflowing Jet
192.	Two Problems On Hypersonic-limit Flow Passing Bodies And Related Numerical Calculations
193.	Analysis Of Transition Flow Characteristics In Hypersonic Inlet And The Effect Of Leading Edge Bluntness
194.	Dynamic Drag Reduction Mechanism Study Of Hypersonic Aircraft
195.	Research On The Aerodynamic Heat And Thermal Effect Of Laser Irradiation Of Hypersonic Aircraft
196.	Numerical Simulation Of Hypersonic Turbulent Flow In Near Space Coupled With High Temperature Gas Effects
197.	Investgation Of Drag And Heat Flux Reduction Mechanism Of Combinational Forward-facing Cavity And Counterflowing Pulsed Jet Configuration
198.	Investigation On The Bi-global Instability Of The Streaky Structures Induced By Fundamental Secondary Instability Modes In A Hypersonic Boundary Layer
199.	Verification Of Local Scattering Theory As Is Applied To Transition Prediction In Hypersonic Boundary Layers
200.	Study On Locally Rarefied Gas Effect Of Hypersonic Flow Based On Direct Simulation Monte Carlo Method
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