Numerical Analysis of Inlet Parameters on the Combustion Performance of Side-Dump Ramjets
碩士 === 國立成功大學 === 航空太空工程學系 === 87 === In the present work, a modified KIVA3 computer program code is used to calculate the three-dimensional transient spray combustion flow-field of ramjet combustors attached symmetrically with four side inlet ducts. Fuel is injected from the four side in...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/71018205702084864201 |