11.07.2015 Views

Modélisation de l'écoulement diphasique dans les injecteurs Diesel

Modélisation de l'écoulement diphasique dans les injecteurs Diesel

Modélisation de l'écoulement diphasique dans les injecteurs Diesel

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

CAV2001:sessionB6.005 10leaves the injector and enters the combustion chamber.The topology of the flow is similar to Soteriou visualizations (see Soteriou 1999), showing alarge vapour pocket attached to the sharp edge inlet, and the cavitation which is located withinthe attached boundary layer.Fig. 6 – Stabilization of cavitation in a single hole orifice. Mixture <strong>de</strong>nsity in g/cm 3 .Consi<strong>de</strong>ring the flowrate exiting from the nozzle, we can remark that, as soon as cavitationreaches the injector exit, the flow behaves as it was “chocked” and the discharge coefficient remainsconstant at C d = 0.62. This result can be compared to Ohrn experimental results (see Ohrnet al. 1991). In fact, the flow remains attached until cavitation reaches the exit, as can be seen infigure 5. This can be clearly seen in figure 10, as the discharge coefficient continues to grow until8 ∗ 10 −6 s. At that time, cavitation reaches the exit and the flow becomes completely <strong>de</strong>tached,leading to a well-known flowrate limitation.These results are in accordance with experimental visualizations and measurements, validatingthe co<strong>de</strong> for a typical injection configuration.5 3D resultsIn or<strong>de</strong>r to have a better un<strong>de</strong>rstanding of the cavitating flow in <strong>Diesel</strong> injector nozzle, one hasto mo<strong>de</strong>l the flow in the whole geometry as reported in Dumont et al. (2000). In this paper arepresented 3D results of cavitation in a single hole sharp-edge injector. The geometry is discretized

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!