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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Pr<strong>in</strong>cipal results: Swirl atomizer<br />
• When liquid pressure drop <strong>in</strong>creases from 1.5 to 5 bars the droplet size<br />
decreases from 110 µm to 60 µm, the size of droplets grows from the spray<br />
center to its periphery whereas their velocity decreases.<br />
• Maximum liquid flux also shifts from the center of the spray to its<br />
periphery.<br />
• The spray angle <strong>in</strong>crease from 75 to 90 degrees with liquid pressure drop<br />
rise.<br />
יום העיון החמישי במנוע<br />
סילון וטורבינות גז<br />
יום ה', א' בחשון תשס"ו,<br />
03/11/2005<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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