Experimental Study of Surface Control Effectiveness in Hyper/Supersonic Low Density Flows
碩士 === 國立臺灣大學 === 應用力學研究所 === 85 === A three-component balance is designed and constructed for shock tunnel hypersonic flows. Static calibration and modal testing reveal that the frequency response of the balance are well above 1kHz,and the...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1997
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| Online Access: | http://ndltd.ncl.edu.tw/handle/35456549940408808449 |