


{"id":398106,"date":"2024-12-20T12:42:59","date_gmt":"2024-12-20T12:42:59","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/les-simulation-of-a-fragment-of-a-hydrogen-air-combustion-chamber\/"},"modified":"2024-12-20T12:42:59","modified_gmt":"2024-12-20T12:42:59","slug":"les-simulation-of-a-fragment-of-a-hydrogen-air-combustion-chamber","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/les-simulation-of-a-fragment-of-a-hydrogen-air-combustion-chamber\/","title":{"rendered":"LES simulation of a fragment of a hydrogen-air combustion chamber"},"content":{"rendered":"<p>&lt;p class=&#8221;MsoNormal&#8221;&gt;&lt;span lang=&#8221;EN-GB&#8221; style=&#8221;mso-ansi-language: EN-GB;&#8221;&gt;I&#8217;m trying to run WMLES simulation of portion of hydrogen-air combustor (single nozzle pair), where hydrogen is injected perpendicularly into air stream, for TCI I&#8217;m using EDC model. At the beginning I would like to add that I&#8217;m not the specialist in LES.&lt;span style=&#8221;mso-spacerun: yes;&#8221;&gt;&nbsp; &lt;\/span&gt;First, I&#8217;ve run the RANS cold flow precursor, where the temperature is limited to air and fuel temperatures. Everything converges nicely. I analyzed the mesh using the integral length scale and densified it in regions where the ratio of integral length scale to grid size is less than 10. Y+ is kept below 1, while x+ and z+ are close to 25. Then I switch to LES, set the second order numerics and the second order bounded time discretization.&lt;span style=&#8221;mso-spacerun: yes;&#8221;&gt;&nbsp; &lt;\/span&gt;Due to the high hydrogen velocities (~160 m\/s) the timestep has to be very low ~ 1e-8 to keep the Courant number below 1. But for the first few simulations I&#8217;m using lower timestep 5e-9. However, when I run simulation, the solution diverges very quickly and triggers floating point error. To prevent from it I reduced to relaxation factors, which helped, but on the other hand solution doesn&#8217;t converge now. &lt;\/span&gt;&lt;\/p&gt;&lt;p class=&#8221;MsoNormal&#8221;&gt;&lt;span lang=&#8221;EN-GB&#8221; style=&#8221;mso-ansi-language: EN-GB;&#8221;&gt;Does anyone have any idea why it diverges so abruptly or any tips how I could fix it? Is the EDC model suitable for use with LES? So far it is only cold flow and it causes so many problems. &lt;\/span&gt;&lt;\/p&gt;&lt;p class=&#8221;MsoNormal&#8221;&gt;&lt;span lang=&#8221;EN-GB&#8221; style=&#8221;mso-ansi-language: EN-GB;&#8221;&gt;Any help would be greatly appreciated.&lt;\/span&gt;&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-398106","topic","type-topic","status-publish","hentry","topic-tag-cfd-combustion","topic-tag-eddy-dissipation-model"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"I&#039;m trying to run WMLES simulation of portion of hydrogen-air combustor (single nozzle pair), where hydrogen is injected perpendicularly into air stream, for TCI I&#039;m using EDC model. At the beginning I would like to add that I&#039;m not the specialist in LES. 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