Numerical Investigation of Nozzle Flow Field in the Thruster of Satellites
碩士 === 國立成功大學 === 航空太空工程學系 === 83 === The numerical method used in this paper is an implicit upwind Total-Variation-Diminishing axi-symmetric Euler/Navier- Stokes( N-S) solver. The results obtained from the two solvers for studying the low-thrust nozzle a...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1995
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| Online Access: | http://ndltd.ncl.edu.tw/handle/59726673896604591670 |