Modeling and Implementation a Hypersonic Wind Tunnel Controller
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 92 === Stagnation Pressure Control is a controller which is used to regulate the mass flow rate of air by an electrically controlled valve to set up a steady flow field in the settling chamber. Basically, a hypersonic wind tunnel experiment is performan...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/55543492087228514227 |