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Yokohama National University Repository >
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5-1 学術雑誌論文 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/10131/3677
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| Title: | Total Analysis of Overall Performance and Axial Thrust of Rocket Pump |
| Author: | Kurokawa, Junichi
Kamijo, Kenjiro
Shimura, Takashi |
| Affiliation: | Yokohama National University Yokohama, Japan
National Aerospace Laboratory Kakuta, Japan
National Aerospace Laboratory Kakuta, Japan |
| Issue Date: | 1991 |
| Publisher: | The American Society of Mechanical Engineers |
| Abstract: | The LOX pump in the first stage of the next large launch vehicle, H-Ⅱ rocket, in Japan showed fairly good results in both the overall performance and thrust balance. However, the behaviour of the axial thrust is not well known because of the complicated flow in the thrust-balancing device. In order to reveal the flow characteristics and to determine the mechanism of thrust balance, the internal flow in every part of the LOX pump is fully analyzed together with the pump overall performance. The analysis developed here is confirmed to give satisfactory results to the pump overall performance and the axial thrust behaviour by comparing with the measurements. |
| URI: | http://hdl.handle.net/10131/3677 |
| ISBN: | 0791807142 |
| Type: | Journal Article |
| Language: | eng |
| NCID: | BA13025110 |
| Journal Title: | Numerical simulations in turbomachinery : presented at the First ASME-JSME Fluids Engineering Conference, Portland, Oregon, June 23-27, 1991 |
| Volume: | 120 |
| Start Page: | 29 |
| End Page: | 34 |
| Version: | publisher |
| Appears in Collections: | 5-1 学術雑誌論文
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Files in This Item:
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Description |
Size | Format |
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| B-056.pdf | | 775Kb | Adobe PDF | View/Open |
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