Fluid flow studies of the F-5E and F-16 inlet ducts
The intake represents the front of a complex aerodynamic system. The shape of the intake diffuser follows the contours of the aircraft for external aerodynamic reasons. However the meandering shape can result in unwanted secondary flow or swirl build up at the Aerodynamic Interface Plane (AIP), resu...
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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2009
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| 在線閱讀: | https://hdl.handle.net/10356/14581 |
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| 機構: | Nanyang Technological University |
| 語言: | English |