| Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor | |
Liu, Mingjiang1; Sun, Mingbo1; Zhao, Guoyan1; Meng Y(孟宇)2,3 ; Huang, Yuhui4; Ma, Guangwei1; Wang, Hongbo1
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| Corresponding Author | Sun, Mingbo([email protected]) ; Zhao, Guoyan([email protected]) |
| Source Publication | AEROSPACE SCIENCE AND TECHNOLOGY
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| 2022-11-01 | |
| Volume | 130Pages:11 |
| ISSN | 1270-9638 |
| Abstract | To investigate the relationship between the thrust performance and combustion mode in a scramjet combustor, the acceleration process of a symmetrical tandem-cavity combustor is numerically investigated based on previous experiments. The numerical results are essentially in agreement with the experimental results through high-speed photography and wall pressure comparisons, which verifies the reliability of the numerical method. Then, three groups of simulations with different equivalent ratios are designed under the condition of inlet flow Mach numbers 2.4, 2.5, 2.6, 2.7, and 2.9. Complete combustion efficiency and specific section thrust are defined to measure the combustion efficiency of kerosene and thrust performance. Four combustion modes are defined and observed in simulations, i.e. strong ram mode, weak ram mode, dual-mode ram mode, and scram mode. The simulation results show that the combustion modes in the former and the later cavities for this tandem-cavity scramjet combustor are related to each other. Combustion modes have a significant impact on the thrust performance of the combustor and the specific section thrust mutation is caused by mode transition. Under different inlet Mach numbers, appropriate equivalent ratio settings can improve thrust performance for this tandem -cavity supersonic combustor. Two ideal combustion modes realized by different injection schemes are proposed for better thrust performance of symmetrical tandem-cavity supersonic combustor.(c) 2022 Elsevier Masson SAS. All rights reserved. |
| Keyword | Tandem-cavity Scramjet combustor Combustion mode Thrust performance |
| DOI | 10.1016/j.ast.2022.107904 |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000882419600001 |
| WOS Keyword | FLAME STABILIZATION ; TRANSITION ; OSCILLATIONS ; MECHANISM ; FLOW |
| WOS Research Area | Engineering |
| WOS Subject | Engineering, Aerospace |
| Funding Project | National Natural Science Foundation of China[11925207] ; National Natural Science Foundation of China[12002381] ; Scientific Research Plan of National University of Defense Technology[ZK19-02] ; Science and Technology Foundation of State Key Laboratory[6142703200311] |
| Funding Organization | National Natural Science Foundation of China ; Scientific Research Plan of National University of Defense Technology ; Science and Technology Foundation of State Key Laboratory |
| Classification | 一类 |
| Ranking | 3+ |
| Contributor | Sun, Mingbo ; Zhao, Guoyan |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/90805 |
| Collection | 高温气体动力学国家重点实验室 |
| Affiliation | 1.Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China; 2.Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China; 3.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China; 4.Equipment Project Management Ctr, Equipment Dev Dept, Beijing 100089, Peoples R China |
| Recommended Citation GB/T 7714 | Liu, Mingjiang,Sun, Mingbo,Zhao, Guoyan,et al. Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2022,130:11.Rp_Au:Sun, Mingbo, Zhao, Guoyan |
| APA | Liu, Mingjiang.,Sun, Mingbo.,Zhao, Guoyan.,孟宇.,Huang, Yuhui.,...&Wang, Hongbo.(2022).Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor.AEROSPACE SCIENCE AND TECHNOLOGY,130,11. |
| MLA | Liu, Mingjiang,et al."Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor".AEROSPACE SCIENCE AND TECHNOLOGY 130(2022):11. |
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| Jp2022FA094.pdf（3841KB） | 期刊论文 | 出版稿 | 开放获取 | CC BY-NC-SA | View Download | |
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