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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| 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 |
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doaj-3ecb1e0e37ce45b68a4da44901bd83532020-11-25T00:02:30ZengKorean Space Science Society (KSSS)Journal of Astronomy and Space Sciences2093-55872093-14091986-06-01312940A Optimal Design of the Rocket Nozzle Wall by the Numerical MethodJin-Won Kim0College of Engineering, Chosun UniversityIt 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 the input data of Tungsten, Graphite, Alumina, Aluminum, Molybdenum, Plastic laminate. The results of the study of the study for pressure of 93.5 kg/cm^2 and temperature of 3000 degC in the nozzle dia of 40 cm are as follows. http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1986/v3n1/OJOOBS_1986_v3n1_29.pdf |
| collection |
DOAJ |
| language |
English |
| format |
Article |
| sources |
DOAJ |
| author |
Jin-Won Kim |
| spellingShingle |
Jin-Won Kim A Optimal Design of the Rocket Nozzle Wall by the Numerical Method Journal of Astronomy and Space Sciences |
| author_facet |
Jin-Won Kim |
| author_sort |
Jin-Won Kim |
| title |
A Optimal Design of the Rocket Nozzle Wall by the Numerical Method |
| title_short |
A Optimal Design of the Rocket Nozzle Wall by the Numerical Method |
| title_full |
A Optimal Design of the Rocket Nozzle Wall by the Numerical Method |
| title_fullStr |
A Optimal Design of the Rocket Nozzle Wall by the Numerical Method |
| title_full_unstemmed |
A Optimal Design of the Rocket Nozzle Wall by the Numerical Method |
| title_sort |
optimal design of the rocket nozzle wall by the numerical method |
| publisher |
Korean Space Science Society (KSSS) |
| series |
Journal of Astronomy and Space Sciences |
| issn |
2093-5587 2093-1409 |
| publishDate |
1986-06-01 |
| description |
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 the input data of Tungsten, Graphite, Alumina, Aluminum, Molybdenum, Plastic laminate. The results of the study of the study for pressure of 93.5 kg/cm^2 and temperature of 3000 degC in the nozzle dia of 40 cm are as follows. |
| url |
http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1986/v3n1/OJOOBS_1986_v3n1_29.pdf |
| work_keys_str_mv |
AT jinwonkim aoptimaldesignoftherocketnozzlewallbythenumericalmethod AT jinwonkim optimaldesignoftherocketnozzlewallbythenumericalmethod |
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