FUM---an efficient MmB solver for steady inviscid flows A fully upwind MmB method FUM is presented for the numerical prediction of hypersonic inviscid flows around shuttle-like bodies. The method is shock-fitting free, singularity-capturing. It is MmB and entropy-satisfying for 1-D scalar conservation laws. Numerical tests show complex flow fields at high angles of attack and high Mach numbers competitive with those obtained using shock-fitting approaches.
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References in zbMATH (referenced in 2 articles , 1 standard article )
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- Liu, T. G.; Khoo, B. C.; Yeo, K. S.: The simulation of compressible multi-medium flow. I: A new methodology with test applications to 1D gas-gas and gas-water cases. II: Applications to 2D underwater shock refraction (2001)
- Wu, H. M.; Yang, M. L.; Hu, C. Q.; Oshima, K.: FUM---an efficient MmB solver for steady inviscid flows (1993)