High-spatial resolution measurements of the velocity field of a supersonic jet impinging on a flat surface were conducted. To study the effect of the boundary condition, two nozzle outer geometries were investigated. The experimental results presented here are for a nozzle pressure ratio of NPR = 3.0 and a nozzle to plate spacing of Z∕D =3.5. The flow fields of the corresponding cases show that although the general features of the flow are similar, the ambient air entrainment into the shear layer is different. This change in entrainment influences the rest of the jet structure.
|Original language||English (US)|
|Title of host publication||Fluid-Structure-Sound Interactions and Control - Proceedings of the 3rd Symposium on Fluid-Structure-Sound Interactions and Control|
|Editors||A.D. Lucey , Yang Liu, Lixi Huang, Yu Zhou|
|Number of pages||5|
|State||Published - 2016|
|Event||3rd Symposium on Fluid-Structure-Sound Interactions and Control,FSSIC 2015 - Perth, Australia|
Duration: Jul 5 2017 → Jul 9 2017
|Name||Lecture Notes in Mechanical Engineering|
|Other||3rd Symposium on Fluid-Structure-Sound Interactions and Control,FSSIC 2015|
|Period||7/5/17 → 7/9/17|
Bibliographical noteFunding Information:
The financial support to conduct this research by the Australian Research Council is gratefully acknowledged. This research was undertaken with the assistance of resources from the National Computational Infrastructure (NCI), which is supported by the Australian Government.
© Springer-Verlag Berlin Heidelberg 2016.
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