Abstract
When we analyze the compressible flow field including shock wave by computational calculation, the solution diverges because of the discontinuity of shock. If we use transformed-Fluid-in-Cell Method, the discontinuity is artificially smoothed and we can analyze the flow field stably. But in the analysis by transformed-Fluid-in-Cell Method, mesh form influences the solution. So we applied the Adaptive Mesh Method to transformed-Fluid-in-Cell Method and got the solution not influenced by mesh form in the analysis of super sonic flow field around blunt nosed body.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
