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Numerical study on the effect of rocket plume to the jet flow deflector in liquid rocket engine test stage
| Content Provider | Scilit |
|---|---|
| Author | Ding, Jiawei Liu, Yongwei He, Hong |
| Copyright Year | 2019 |
| Description | Journal: Journal of Physics: Conference Series Jet flow deflector is one of the most important facility in liquid rocket engine test stage. It is necessary to investigate the effect of rocket plume to the jet flow deflector. Based on the theory of computational fluid dynamics, the flow field of a rocket engine plume is simulated and analysed by numerical method. The velocity field and temperature field of the plume in rocket engine test are obtained. The structural characteristics of engine plume flow field and the impact effect on flow deflector are analysed. Finally, results are applied to the thermal protection design of the test stage. |
| Related Links | https://iopscience.iop.org/article/10.1088/1742-6596/1300/1/012052/pdf |
| ISSN | 17426588 |
| e-ISSN | 17426596 |
| DOI | 10.1088/1742-6596/1300/1/012052 |
| Journal | Journal of Physics: Conference Series |
| Issue Number | 1 |
| Volume Number | 1300 |
| Language | English |
| Publisher | IOP Publishing |
| Publisher Date | 2019-08-01 |
| Access Restriction | Open |
| Subject Keyword | Journal: Journal of Physics: Conference Series Aerospace Engineering Rocket Plume Flow Deflector Engine Test Jet Flow Rocket Engine |
| Content Type | Text |
| Resource Type | Article |
| Subject | Physics and Astronomy |
