2009
DOI: 10.1016/j.ijheatmasstransfer.2009.03.060
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The influence of rotational charge motion intensity on nitric oxide formation in gas-engine cylinder

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Cited by 16 publications
(6 citation statements)
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“…The initial value of turbulent kinetic energy k0 = 5 m 2 /s 2 , and turbulence length scale TLS0 = 0.001 m As a result of the calculation, the values of temperature, pressure, and velocities of the working fluid in the cross-sections of the WE working chamber were obtained both for the processes of exhaust, scavenging, filling of the working chamber (Figure 6a-c), and combustion of the fuel-air mixture (Figure 7a-d). It is worth noting that in traditional piston engines, an increase in the efficiency of the combustion of the air-fuel mixture, as well as a reduction in emissions of harmful substances, can be achieved by profiling the intake ports and the combustion chamber [20][21][22]. In a Wankel engine, the effect of flow swirl at the inlet is less noticeable due to the characteristic shape of the combustion chamber, which, by the time the rotor reaches the TDC (top dead center, the point of the minimum combustion chamber volume), is strongly deformed in the radial direction.…”
Section: Results Of Numerical Experimentsmentioning
confidence: 99%
“…The initial value of turbulent kinetic energy k0 = 5 m 2 /s 2 , and turbulence length scale TLS0 = 0.001 m As a result of the calculation, the values of temperature, pressure, and velocities of the working fluid in the cross-sections of the WE working chamber were obtained both for the processes of exhaust, scavenging, filling of the working chamber (Figure 6a-c), and combustion of the fuel-air mixture (Figure 7a-d). It is worth noting that in traditional piston engines, an increase in the efficiency of the combustion of the air-fuel mixture, as well as a reduction in emissions of harmful substances, can be achieved by profiling the intake ports and the combustion chamber [20][21][22]. In a Wankel engine, the effect of flow swirl at the inlet is less noticeable due to the characteristic shape of the combustion chamber, which, by the time the rotor reaches the TDC (top dead center, the point of the minimum combustion chamber volume), is strongly deformed in the radial direction.…”
Section: Results Of Numerical Experimentsmentioning
confidence: 99%
“…We also emphasize that this mathematical model is typical for CFD calculations of processes in piston engines and it is described in detail by Merker et al [16], Basshuysen and Schäfer [17], Kavtaradze et al [18].…”
Section: Numerical Analysismentioning
confidence: 99%
“…We also emphasize that this mathematical model is typical for CFD calculations of processes in piston engines and it is described in detail in Merker et al 2019;Basshuysen and Schäfer 2007;Kavtaradze et al 2009).…”
Section: Mathematical Modelmentioning
confidence: 99%