Innovations in Hypersonic Flow Simulation

摘要：

Impressive and broad-base technical progresses have been made in high-speed propulsion and power generation over past decades. At the transient state of major hypersonic programs worldwide, it will be invaluable to assess the-state-of-art advances and to project scientific needs for future attainment. The computational model and simulation capability for hypersonic flow is an interdisciplinary endeavor and has a very rich content in rarefied gasdynamics, high-speed fluid dynamics, nonequilibrium chemical kinetics, chemical-physics, radiative energy transfer, and ablation. The knowledge base is extremely vast for any individual to be very well versed. To avoid significant omission, the present discussion is limited to the topics of numerical algorithm development, nonequilibrium chemicalphysics, and the plasma actuators for flow control.

关键词： Hypersonic Numerical algorithm Chemical-physical kinetics Plasam acuator

作者: J. S. Shang

作者单位: Mechanical & Materials Engineering Department Wright State University Dayton, USA

会议类型: 国际会议

会议名称: 4th International Symposium on Jet Propulsion and Power Engineering(第四届喷气推进与动力工程国际会议 ISJPPE2012)

会议地点: 西安

会议语种:英文

页码: 339-351

在线出版日期: 2012-09-10（万方平台首次上网日期，不代表论文的发表时间）