Flow Characterization of the T3 Hypersonic Shock TunnelD Romanelli Pinto, T V C Marcos,Victor Alves Barros Galvao,A C Oliveira, J B Chanes,M A S Minucci,P G P Toromag(2012)引用 2|浏览3暂无评分关键词Mach Number, Test Section, Shock Tube, Nozzle Exit, Shock TunnelAI 理解论文溯源树样例生成溯源树,研究论文发展脉络Chat Paper正在生成论文摘要