Calibration of exit velocity and temperature distribution for subsonic jet flow
Tabs have been known for a long time to have the capability to eliminate screech noise from supersonic jets. It is this application that has provided the most motivation for the subsequent studies on the effects of tabs have on jets. This Final Year Project is aimed to reproduce and calibrate the a...
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| 主要作者: | |
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2009
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/16724 |
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| 機構: | Nanyang Technological University |
| 語言: | English |