A Optimal Design of the Rocket Nozzle Wall by the Numerical Method
It is the aims of this study to choose the materials and determine the material thickness of laminated Rocket Nozzle Wall operating at high pressure and high temperature. The heat conduction analysis of each layer was performed by Crank Nicolson method changing the thickness and the materials for th...
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| Format: | Article |
| Language: | English |
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Korean Space Science Society (KSSS)
1986-06-01
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| Series: | Journal of Astronomy and Space Sciences |
| Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1986/v3n1/OJOOBS_1986_v3n1_29.pdf |