The Analysis of the Instability in a Rocket Combustor by Acoustic Cavity Simulation
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 98 === In the liquid rocket propulsion, the combustion instability may severely damage the system. This research focused on the design analysis of the suppression mechanism for combustion instabilities using acoustic simulations. The model combustors with variab...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2010
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Online Access: | http://ndltd.ncl.edu.tw/handle/75676346573667890199 |