fuel injection and combustion processes in small jet engines
fuel injection and combustion processes in small jet engines
fuel injection and combustion processes in small jet engines
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3 Droplet size: comparison with other studies<br />
SMD, micron<br />
120<br />
100<br />
80<br />
60<br />
40<br />
20<br />
0<br />
Present<br />
study<br />
Axial swirler<br />
Rizkalla's data<br />
Radial swirler<br />
0 50 100 150<br />
Air velocity, m/s<br />
Rizkalla et. al.<br />
The effect of air velocity <strong>in</strong> our study was weaker. However “our”<br />
droplets have <strong>small</strong>er diameter for low air velocities<br />
יום העיון החמישי במנוע<br />
סילון וטורבינות גז<br />
יום ה', א' בחשון תשס"ו,<br />
03/11/2005<br />
Comparison of air velocity effect on SMD for<br />
present study <strong>and</strong> Rizkalla's <strong>and</strong> Lefebvre's data<br />
Turbo <strong>and</strong> Jet<br />
Eng<strong>in</strong>e Laboratory<br />
Technion – Israel<br />
www. <strong>jet</strong>-eng<strong>in</strong>e-lab.technion.ac.il
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