27.12.2013 Views

Etude de la combustion de gaz de synthèse issus d'un processus de ...

Etude de la combustion de gaz de synthèse issus d'un processus de ...

Etude de la combustion de gaz de synthèse issus d'un processus de ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

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

Numerical simu<strong>la</strong>tion of a syngas-fuelled engine<br />

Figures 6.9-6.10 show that the adapted co<strong>de</strong> is able to reproduce fairly good the RCM<br />

in-cylin<strong>de</strong>r pressure. Main discrepancies are found in the <strong>combustion</strong> phase especially<br />

for short ignition timings. On the expansion phase, pressure curve come back to match<br />

with experimental result fairly well. These discrepancies can be exp<strong>la</strong>ined from both the<br />

experimental and numerical results. From the experimental point of view, RCM<br />

leakages, which correspond to mass losses especially at elevated pressures, can be a<br />

reasonable cause for the lower pressures. From the numerical point of view, there are<br />

various factors that can be source of errors due to the co<strong>de</strong> adaptation to the RCM<br />

characteristics, namely:<br />

tel-00623090, version 1 - 13 Sep 2011<br />

- The heat transfer coefficient that was tested on the compression stroke with<br />

very good performance, however it <strong>la</strong>cks of verification for the expansion stroke.<br />

- The turbulence intensity used on the burning rate mo<strong>de</strong>l was tacked from<br />

experimental results of the single compression, thus it <strong>la</strong>cks of verification for<br />

the expansion stroke;<br />

- Other minor errors like the in-cylin<strong>de</strong>r volume polynomial fitting and the<br />

equivalent rotation speed. The <strong>la</strong>tter directly affects the heat transfer coefficient.<br />

6.4. Syngas fuelled-engine<br />

For small scale cogeneration units (

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

Saved successfully!

Ooh no, something went wrong!