线 发表于 2025-4-1 03:02:45
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Local Preconditioning Techniques Coupled with a Variational Multiscale Method to Solve Compressible e evaluate this methodology simulating a steady flow over the NACA 0012 airfoil under some regimes of inflow Mach numbers. The numerical result exhibits promising solutions to compressible flow problems in the incompressible limit.话 发表于 2025-4-1 13:52:29
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