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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T E S T R E S U L T S<br />
3. Axial droplet velocity<br />
No air 44m/s 68m/s 115m/s<br />
Axial velocity, m<br />
25<br />
20<br />
15<br />
10<br />
5<br />
0<br />
0 10 20 30<br />
Radius, mm<br />
Radial<br />
•MAXIMUM DROPLET VELOCITY IS NEAR THE CENTRE OF THE SPRAY.<br />
• FOR THE SAME LIQUID PRESSURE, THE DROPLETS VELOCITY ARE HIGHER FOR<br />
AIRBLAST ATOMIZER<br />
יום העיון החמישי במנוע<br />
סילון וטורבינות גז<br />
יום ה', א' בחשון תשס"ו,<br />
03/11/2005<br />
Axial spray velocity distribution for air-blast<br />
atomizer with radial swirler<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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