Transient Spray Cone Angles in Pressure-Swirl Injector Sprays

2004-01-2939

10/25/2004

Event
2004 Powertrain & Fluid Systems Conference & Exhibition
Authors Abstract
Content
The transient cone angle of pressure swirl sprays from injectors intended for use in gasoline direct injection engines was measured from 2D Mie scattering images. A variety of injectors with varying nominal cone angle and flow rate were investigated. The general cone angle behavior was found to correlate well qualitatively with the measured fuel line pressure and was affected by the different injector specifications. Experimentally measured modulations in cone angle and injection pressure were forced on a comprehensive spray simulation to understand the sensitivity of pulsating injector boundary conditions on general spray structure. Ignoring the nozzle fluctuations led to a computed spray shape that inadequately replicated the experimental images; hence, demonstrating the importance of quantifying the injector boundary conditions when characterizing a spray using high-fidelity simulation tools.
Meta TagsDetails
DOI
https://doi.org/10.4271/2004-01-2939
Pages
10
Citation
Snyder, J., Grover, R., Sick, V., and Assanis, D., "Transient Spray Cone Angles in Pressure-Swirl Injector Sprays," SAE Technical Paper 2004-01-2939, 2004, https://doi.org/10.4271/2004-01-2939.
Additional Details
Publisher
Published
Oct 25, 2004
Product Code
2004-01-2939
Content Type
Technical Paper
Language
English