Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles

• المؤلفون الرئيسيون: Meng, Z, Yang, L, Shu, C, Hu, F, Wang, D, Zhang, W
• مؤلفون آخرون: MECHANICAL ENGINEERING
• التنسيق: Conference or Workshop Item
• منشور في: 2020
• الموضوعات: Finite volume method; Flight simulators; Hypersonic flow; Hypersonic vehicles; Inductively coupled plasma mass spectrometry; One dimensional; Shock waves; Central difference method; Computational robustness; Flight vehicles; Lattice boltzmann; Numerical dissipation; One-dimensional lattice; Strong shock waves; Switch function; Navier Stokes equations
• الوصول للمادة أونلاين: https://scholarbank.nus.edu.sg/handle/10635/178076
• المؤسسة: National University of Singapore

10.1088/1742-6596/1053/1/012073