Publication Date:
2019-06-28
Description:
The atomization of several general aviation piston engine manifold port fuel injectors was investigated. The injectors were installed in a test rig and operated under simulated conditions. Laser interferometric techniques were used to optically probe the spray droplet fields for droplet size and velocity at numerous spatial locations throughout the field.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-CR-165200
,
SDL-80-2122-13F
Format:
application/pdf
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