摘要 : Flow and noise fields are explored for the concept of distributed propulsion. A model-scale experiment is performed with an 8:1 aspect ratio rectangular nozzle that is divided into six passages by five septa. The septa geometries ... 展开
作者 | JE Bridges KBMQ Zaman |
---|---|
作者单位 | |
期刊名称 | 《International Journal of Aeroacoustics》 |
总页数 | 16 |
语种/中图分类号 | 英语 / O42 |
关键词 | Jet noise nozzles streamwise vortices turbulence |
馆藏号 | N2008EPST0010671 |