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Kunz[18-20], as representative, constructed a preconditioned, homogenous, multiphase, unsteady Reynolds Averaged Navier-Stokes scheme (RANS), and developed a Computational Fluid Dynamics (CFD) method to simulate the supercavitating flow.
Multiphase CFD modeling of developed and supercavitating flows[R], Supercavitating Flow, von Karman Institue, Brussels Belgium, 2001, 269-312
The numerical simulation of supercavitatoin around projectiles from subsonic to supersonic[J], Journal of Projectiles, Rockets, Missiles, and Guidance, 2009, 29, 5, 166-169(in Chinese)
Dynamic processes of supercavitation and computer simulation[R], Supercavitating Flow, von Karman Institue, Brussels Belgium, 2001, 239-268
Computer simulation of unsteady supercavitating flows[R], High Speed Body Motion in Water, Kiev, Ukraine, 1997, 225-234

Yang Institute of Hydraulic Engineering ,Xi’an University of Technology,Xi’an, China wei_wenli@126.com Keywords: characteristics; CFD simulation; Water drop falling Abstract: In this paper, a numerical two-phase flow model combining with the Realizable k–ε turbulent model for compressible viscous fluid is presented for the computation of water drop falling characteristics; and the equations are solved with the finite volume method.
The results of this simulation are presented in Figs.3.

The simulation is carried out with the free stream velocity of 0.6 M, pressure of 1 bar, and air density 1.225 kg/m3 at 5 0 angle of attack by using FLUENT software.
CFD analysis of the wing in the high transonic speed shows that the morphing in chordwise can make a significant contribution to the critical mach number as shown in Fig.6.
CFD results indicated the maximum mach number reduces with the chord increasing.

NOx and Soot Emissions Numerical Simulation of Diesel Engine Fueled with Biodiesel Jianlin Ge1,a, Dong Tang2,b, Huan Chen3,c, Shengji Liu4,d 1,2,3,4School of Automobile, Jiangsu University, Zhen Jiang 212013, China agjl465893@qq.com, bdtang@ujs.edu.cn, c371045690@qq.com,dliushengji@126.com Key words: Non-road diesel; Bio-diesel; Emission; Numerical Simulation Abstract: The three dimensional numerical simulation on NOx and soot emissions was carried out on 186 FA diesel engine fueled with pure diesel and B20 fuel using CFD software Fire v2008 and the generating rule and distribution of NOx and soot of two fuel was described.
There has been a lot of research on bio-diesel at home and abroad, mainly in the aspect of bio-diesel combustion and spray characteristics[1-3], but it’s less in research on multi-dimensional numerical simulation of bio-diesel engine blends.
In this paper, it was carried out on small biodiesel blended using AVL's FIRE software with diesel combustion process simulation and numerical analysis of their emissions, improving emissions and verifying it according to the conclusions.
Mesh Set up and Calculation Model Use air-cooled diesel engine 186FA-type prototype for the simulation, the main technical parameters in Table 1.
The tests show that Bosch smoke opacity of B0 fuel and B20 fuel is 1.6 and 1.9 respectively, at full speed and full load, and the results are the same as the simulation predicted results.

Combustion Simulation on Fuel oil-mixture gas Converter Based on FLUENT Jiachao Yan a , Shuai Shao and Chengzhe Jin Shenyang Ligong University, Shenyang, China, 110159 ayanjc01@sina.com Key words：Heavy oil exploitation; converter; combustion simulation Abstract.
(11) The simulation analysis  of  combustion chamber components transmission and  gascombustion ANSYS FLUENT analysis software which is a universal CFD software used to simulate complex flow of the range of  incompressible to compression. 
The simulations results show that the combustion chamber design meet the technical requirements.
Based on ANSYS FLUENT analysis software,the components transmission and gas combustion simulation to the combustion chamber in fuel-the mixture  converter.The simulation results of a series of simulation get chart, such as temperature contour map and mix specific heat contour map. 
The mean temperature (468.4359K) and velocity (490.4908m/s) of the exit are confirm in the simulation analysis.The simulation result, determine the combustion chamber design meet the design requirements.

This paper presents numerical simulations on two assembly modification methods for one annular casing.
Fig. 1 Original pump Fig. 2 Flow passage of the original pump Fig. 3 Schematic for casings of method one Fig. 4 Schematic for casing of method two CFD Simulation Mesh Details.
Simulation Settings.
Simulation settings are listed in Table 1.
Fig. 6 shows efficiency comparison between experimental results (given by some factory) and simulation results, which proved that these simulations could provide reasonable prediction for hydraulic performance.

Simulation Study on the Radiant Tube Transferring Characteristics for the Gas-infrared Heated System Daying Zhang1,a, Weidong Zhuang1,band Keqin Gong2,c 1College of Engineering, Heilongjang Bayi Agricultural University, Daqing 163319, China 2Civil Engineering College, Northeast Petroleum University, Daqing 163318, China azdy004@163.com, b81nd@163.com, Cgkqdqpi@126.com Keywords: Gas-fired radiant heating, Numerical simulation, Temperature distribution Abstract.
The numerical simulation for radiant tube heat transferring process of the gas-infrared heated room was finished.
Physics Model of Building A numerical simulation on a gas heating plant was processed.
CFD software is adopted to simulate the indoor temperature field, and the indoor temperature distribution of this plant are shown in Fig.1~ Fig.6.

The size of this simulation area is 200 mm × 30 mm, as shown in Fig. 2.
The simulation area is divided by the software Gambit.
The Computational Fluent Dynamics (CFD) software Fluent is used to set the boundary conditions.
The standard k-ε model is used in the simulation.
After 5954 iterations, the simulation converges.

The unsteady aerodynamics associated with this microrobot was studied by using the method of computational fluid dynamics (CFD).
On the basis of numerical simulation, the Fluid-Structure coupling mechanics for flexible flapping-wings were studied and discussed.
According to the practically developed flapping-wing microrobot, a 2-D simulation model for flexible flapping-wings was established.
In the foundation of the numerical simulation, the variations of different parameters of the flapping microrobot were investigated, such as flapping amplitude, pitch amplitude and flapping frequency.
Finally wind tunnel experiments and flying test verified results of numerical simulation.

Numerical arithmetic, which based on CFD method and is used for design configuration and shape of an icing prober is given.
First, build numerical method for design based on the CFD method; Second, develop the advanced ice sensors according to the optical property of ice; Third, design the aerodynamic shape of the prober to assemble the ice sensor.
Fig.3 Configuration of the prober and the sketch of the wind turbine installed with the prober Simulation of Detection Effects.
The diameter of water droplet for simulation is 20μm, 40μm and 100μm.