DSMC - Globe Thesis - Globe Thesis

Keyword [DSMC] Result: 41 - 60 \| Page: 3 of 5
41.	DSMC Simulation Of Convective Heat And Mass Transfer Between Fine Particles And Gases
42.	Research On N-S/DSMC Hybrid Algorithm In The Transitional Domain
43.	Research On Numerical Simulation Of Attitude Control Rocket Engine Plume
44.	Study Of Stability Of Lubricant Layer And Gas Bearing In Large Capacity Hard Disk Drives Based On MD And DSMC Method
45.	Nozzle Trans-regime Flow Simulation Based On N-S/DSMC Coupling Algorithm
46.	Numerical Research On Aeroforce And Aerothermal Characteristic Of Mechanical Deployable Reentry Vehicle
47.	Plume Simulation Of High-Altitude Solid Rocket Motor Considering Phase Transition And Radiation
48.	SPT Lifetime Improvement Method Based On The Sputtering Resistance Of Diamond
49.	Research On Aerodynamic Characteristics Of Lateral Jet In Hypersonic Flow By The DSMC Method
50.	A Study On The Efficient Microcosmic Algorithm For Multscale Combustion
51.	Numerical Simulation Of Engine Jet Diversion Flow Field Under Vacuum Environment
52.	Utilization Of DSMC Method And Bridging Relation For Transitional Regime Aerodynamics Of Long-range Shells And Rockets
53.	DSMC Calculation Of Hypersonic Rarefied Flows And Research Of Aerodynamic Thermal Engineering Method
54.	Numerical Study On The Influence Of Vacuum Condition In Liquid Evaporation
55.	Numerical Simulation Of Dust Removal Characteristics Of Wire-tube Type Rare Earth Tungsten Cathode High-temperature Electrostatic Precipitator Based On CFD-DSMC
56.	Reduction of rocket-borne atmospheric density measurements using Monte Carlo simulation
57.	Numerical investigation of the effects of continuum breakdown on hypersonic vehicle surface properties
58.	Direct simulation Monte Carlo modeling of condensation in supersonic plume expansions of small polyatomic systems
59.	Micro/nano fins for single phase heat transfer enhancement and development of heat flux boundary condition for DSMC-I
60.	Assessment of gas-surface interaction models for computation of rarefied hypersonic flows
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