Design and testing of a hypersonoic nozzle for a pilot hypersonic shock tunnel
碩士 === 國立成功大學 === 航空太空工程學系 === 82 === A hypersonic nozzle designed by the minimum length nozzle method and incorporated with a boundary layer correction method has been designed and tested at the Shock Tube Facility of Insitute of Aeronau...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1994
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| Online Access: | http://ndltd.ncl.edu.tw/handle/56300146978346141698 |