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Fuel injector characterization studiesThe 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.
Document ID
19810006488
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Houser, M. J.
(Spectron Development Labs., Inc. Costa Mesa, CA, United States)
Bachalo, W. D.
(Spectron Development Labs., Inc. Costa Mesa, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SDL-80-2122-13F
NASA-CR-165200
Report Number: SDL-80-2122-13F
Report Number: NASA-CR-165200
Accession Number
81N15003
Funding Number(s)
CONTRACT_GRANT: NAS3-21288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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