supersonic - Globe Thesis

Keyword [supersonic] Result: 21 - 40 \| Page: 2 of 10
21.	Development Of Numerical Method And Investigation On Performances Of Supersonic Ejectors
22.	A Theoretical And Experimental Study Of Heat And Mass Transfer Characteristics Of Multi-Component Condensing Gas Supersonic Flows
23.	Research Of Static Characteristic For Externally Pressurized Gas Bearing By Highter Supply Pressure
24.	Numerical Research On Supersonic/Hypersonic Plasma Flow And Its Electromagnetic Characteristics
25.	Non-Equilibrium Phase Change And Shock Effect In Supersonic Steam Flow
26.	Fine Numerical Simulation/Experimental Study On High Speed Flow And Aero-Optics Application
27.	Implementation Of Reduced Chemical Kinetics Of Hydrocarbon Fuels And In Situ Adaptive Tabulation In Parallel Computations Of Supersonic Combustion
28.	Research On Form Surface Aerodynamic Optimization Method Of Ramjet Assisted Range Projectile Inlet
29.	Mechanism Study Of Fine Structures And Aero-Optical Effects Of Supersonic Flow Around An Optical Dome
30.	Research On Curved Compression System In Supersonic/Hypersonic Non-uniform Inflow
31.	Investigation Of Validation, Modeling And Application Of Flamelet Model In Supersonic Turbulent Combustion
32.	Experimental Investigation Of Supersonic Boundary Layer And Shock Wave/Boundary Layer Interaction
33.	Numerical Simulation And Experimental Investigation Of The Mixing And Reacting Mechanisms Associated With The Transverse Injection In HYLTE Nozzle
34.	Numerical And Experimental Investigation Of Fuel Spray In Supersonic Cross Flow
35.	Thermal-Fluid-Structure Coupled Analysis Of The Supersonic Conformal Dome
36.	The Local Flow Piston Theory-based Unit Fit Flutter Analysis Aeroservoelastic
37.	Study On Supersonic Atomization Theory And Production Of Solder Alloy Fine Powder
38.	A Numerical Study Of The Evolution Of The Disturbance In 2-D Supersonic Boundary Layer With Pressure Gradient
39.	Calculation For A Three-dimensional Jets Flowfield Of The Rocket
40.	Investigation On Design Of Altitude Control System Of The Missile With Supersonic Speed At Minimum Altitude
<<First <Prev Next> Last>> Jump to