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A computational fluid dynamic (CFD) analysis and an experiment on single cylinder engine test bed of combustion process in a compressed natural gas direct injection (CNGDI) engine with compression ratio 14:1 have been conducted by Abdullah et. al. [3], concluding that a proper heat transfer mechanism was needed to avoid engine malfunction.
Simulation was conducted for all engine speeds on three types of pistons namely the uncoated piston crown, tin (Na2SnO3) coated piston crown and ceramic based yttria partially stabilised zirconia (YPSZ) coated .

., Goh, F.C.The CFD simulation on thermal comfort in a library building in the tropics, 2nd International Symposium on Computational Mechanics, ISCM II, 2010,1233( PART 1): 1529-1534

Kouichi, A simulation model for the pyrolysis of orimulsion, Energy Fuels. 11 (1997), pp. 819-824
Lettner, CFD modelling of external heated pyrolysis of wood chips, 14th European Biomass Conference.

Backreedy [10]has used CFD software to make the simulation study of raw material coke and pulverized coal combustion reaction process.

Due to its simplicity and be directly processed by the graphics hardware, triangle representation scheme has been a standard for representing polyhedral solids in CAD, virtual reality and simulation modeling areas.
Ge, Physics-driven CFD modeling of complex anatomical cardiovascular flows - A TCPC case study, Annals of Biomedical Engineering. 33 (2005) 284-300

Along some FSI simulation performed for the reference design shown in Fig. 5 it has been shown, that even for wings with a small span the deflection as shown in Fig. 7 (left) can be remarkable.
Numeric validation performed has been based on a major simulation environment consisting of CAD, CFD and FE software.
Simulations were performed for a variety of flight conditions and parameters.
What those results show as well as a variety of other simulation Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05 Time [sec] W Time [sec] W Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05Inverse Zimmerman Original Zimmerman Inverse Zimmerman Original Zimmerman 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV Rigid wing MAV Flexible wing MAV Individual Spar Rotation Angle Individual Spar Rotation Angle results described in [3] show is that the flexible MAV wing provides better stability compared to a rigid MAV wing.
To compare the performance between a conventional MAV steered by a rudder and the vector thrust steered alternative an analytic simulation model has been applied which has been described in further detail in [3].

Nore et al. [20] indicates that the proportionality factor, called the incident rainfall coefficient, is a function of the terrain characteristics and of the building itself, and can be determined from experimental results or simulations with computational models of fluid mechanics (CFD).

[6] Mostafazadeh-Fard, Saman, Dissipating Culvert End Design for Erosion Control Using CFD Platform FLOW-3D Numerical Simulation Modeling, Journal of pipeline systems engineering and practice. 14 (2022) 04022064

Ramakrishnan, CFD simulation and experimental validation studies on hydrocyclone, Miner.

Wang [8] has verified using CFD simulation and tests that the emitter prototypes and emitter amplifier model designed based on Froude model law have similar pressure-discharge relationship and pressure distribution along the flow channel.