[Analysis Case] Supersonic Flow Analysis Around Wings 'CONVERGE'
It is published that shock waves can be predicted with very high resolution by AMR.
In "CONVERGE," the Adaptive Mesh Refinement (AMR) feature allows the solver to automatically control the appropriate mesh based on the gradient of the analysis variables. This example demonstrates the analysis of supersonic flow fields around a wing calculated using "CONVERGE," showing that shock waves can be predicted with very high resolution thanks to AMR. 【Features】 - The solver automatically controls the appropriate mesh based on the gradient of the analysis variables. - Shock waves can be predicted with very high resolution due to AMR. *For more details, please refer to the PDF document or feel free to contact us.*
- Company:IDAJ
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