Research on nozzle performance in scramjet

摘要：

The paper studies the influence of geometric parameters upon nozzle performance in scramjet. The geometric parameters include divergent angle, nozzle total length, height ratio, and cowl angle. The research conclusions provide instruction for the choice of geometric parameters in the nozzle design.

关键词： Scramjet Nozzle Performance Numerical simulation Geometric parameters

作者: J.P.Li W.Y.Song Y.Xing

作者单位: School of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China

会议类型: 国际会议

会议名称: The Fifth International Conference on Fluid Mechanics(第五届国际流体力学会议)

会议地点: 上海

会议语种:英文

在线出版日期: 2007-08-15（万方平台首次上网日期，不代表论文的发表时间）