| Citation: | LUO Jiamao, YOU Jin, JIAO Si, et al. Numerical study on heat exchange performance for three-dimensional methane pre-cooler[J]. Journal of Aerospace Power, 2024, 39（8）：20220603 doi: 10.13224/j.cnki.jasp.20220603
|
A three-dimensional simulation method was established to assess the heat exchange performance with methane as coolant for an axial tube-bundled pre-cooler. The flow field of the pre-cooler was obtained at different coolant equivalent ratios and flight conditions, and the control strategy of coolant massflow was proposed from the simulation results. The assessed results indicated that the incoming air could be cooled 131 K at maximum under the condition of three times the equivalent ratio by methane pre-cooler, extending the working velocity spectrum to
| [1] |
WANG Zhenguo,WANG Yuan,ZHANG Jianqiang,et al. Overview of the key technologies of combined cycle engine precooling systems and the advanced applications of micro-channel heat transfer[J]. Aerospace Science and Technology,2014,39: 31-39. doi: 10.1016/j.ast.2014.08.008
|
| [2] |
VARVILL R,BOND A. A comparison of propulsion concepts for SSTO reusable launchers[J]. Journal of the British Interplanetary Society,2003,56: 108.
|
| [3] |
OIKE M,KAMIJO K,TANAKA D,et al. LACE for rocket-based combined-cycle: AIAA1999-0091 [R]. Reston,US: AIAA,1999.
|
| [4] |
ANDREW C,ADAM W,JASON A,et al. ACES: propulsion technology for next generation space transportation: IAC-03-S. 5.03 [R]. Bremen,Germany: AIAA,2003.
|
| [5] |
SATO T,TANATSUGU N,NARUO Y,et al. Development study on ATREX engine[J]. Acta Astronautica,2000,47(11): 799-808. doi: 10.1016/S0094-5765(00)00129-6
|
| [6] |
SAWAI S,SATO T,KOBAYASHI H,et al. Flight test plan for ATREX engine development: AIAA-2003-7027 [R]. Norfolk,US: AIAA,2003.
|
| [7] |
SATO T,KOBAYASHI H,TANATSUGU N,et al. Development study of the precooler of ATREX engine: AIAA-2003-6985[R]. Norfolk,US: AIAA,1997.
|
| [8] |
HARADA K,TANATSUGU N,SATO T. Development study of a precooler for the air-turboramjet expander-cycle engine[J]. Journal of Propulsion and Power,2001,17(6): 1233-1238. doi: 10.2514/2.5869
|
| [9] |
FUKIBA K,INOUE S,OHKUBO H,et al. New defrosting method using jet impingement for precooled turbojet engines[J]. Journal of Thermophysics and Heat Transfer,2009,23(3): 533-542. doi: 10.2514/1.40491
|
| [10] |
张蒙正,李平,陈祖奎. 组合循环动力系统面临的挑战及前景[J]. 火箭推进,2009,35(1): 1-8,15. ZHANG Mengzheng,LI Ping,CHEN Zukui. Challenge and perspective of combined cycle propulsion system[J]. Journal of Rocket Propulsion,2009,35(1): 1-8,15. (in Chinese doi: 10.3969/j.issn.1672-9374.2009.01.001
|
| [11] |
LONGSTAFF R,BOND A. The SKYLON project: AIAA-2011-2244 [R]. San Francisco,USA: AIAA,2011
|
| [12] |
VARVILL R,BOND A. The Skylon spaceplane: progress to realization[J]. Journal of the British Interplanetary Society,2008,61: 412-418.
|
| [13] |
European Space Agency. Skylon assessment report [R]. Paris,France: European Space Agency,2011.
|
| [14] |
MURRAY J J,GUHA A,BOND A. Overview of the development of heat exchangers for use in air-breathing propulsion pre-coolers[J]. Acta Astronautica,1997,41(11): 723-729. doi: 10.1016/S0094-5765(97)00199-9
|
| [15] |
MURRAY J,HEMPSELL C,BOND A. An experimental precooler for airbreathing rocket engines[J]. Journal of the British Interplanetary Society,2001,54: 199-209.
|
| [16] |
WEBBER H,FEAST S,BOND A. Heat exchanger design in combined cycle engines[J]. Journal of the British Interplanetary,2008,54: 1-6.
|
| [17] |
VARVILL R. Heat exchanger development at Reaction Engines Ltd.[J]. Acta Astronautica,2010,66(9/10): 1468-1474.
|
| [18] |
WEBBER H,TAYLOR N. Tunnel development for heat transfer analysis in compact heat exchangers: AIAA-2010-4537[R]. Chicago,USA: AIAA,2010.
|
| [19] |
高远,陈玉春,史新兴. SABRE预冷器计算模型及其在整机模型中的应用[J]. 推进技术,2021,42(11): 2485-2493. GAO Yuan,CHEN Yuchun,SHI Xinxing. SABRE precooler calculation model and its application in engine model[J]. Journal of Propulsion Technology,2021,42(11): 2485-2493. (in Chinese
|
| [20] |
李帅,马同玲,刘洪涛,等. SABRE预冷器结构参数对其性能影响的数值分析[J]. 推进技术,2022,43(4): 257-264. LI Shuai,MA Tongling,LIU Hongtao,et al. Numerical analysis of effects of pre-cooler structure parameter on its performance in SABRE[J]. Journal of Propulsion Technology,2022,43(4): 257-264. (in Chinese
|
| [21] |
张小平,李春红,马冬英. 液氧/甲烷发动机动力循环方式研究[J]. 火箭推进,2009,35(4): 14-20,43. ZHANG Xiaoping,LI Chunhong,MA Dongying. Study on the LOX/methane rocket engine power cycles[J]. Journal of Rocket Propulsion,2009,35(4): 14-20,43. (in Chinese doi: 10.3969/j.issn.1672-9374.2009.04.003
|
| [22] |
王成刚,孙宝坤,林纬,等. 超临界压力下低温甲烷在螺旋管内传热数值研究[J]. 低温与超导,2018,46(2): 1-5,14. WANG Chenggang,SUN Baokun,LIN Wei,et al. Heat transfer study of methane in a helical coiled tube at supercritical pressure[J]. Cryogenics & Superconductivity,2018,46(2): 1-5,14. (in Chinese
|
| [23] |
张楚薇. 液氧甲烷发动机燃烧及耦合传热计算研究[D]. 北京: 中国航天科技集团公司第一研究院,2017. ZHANG Chuwei. Study on the coupled calculation of combustion and heat transfer in LOX/methane rocket engine[D]. Beijing: China Aerospace Science and Technology Corporation,2017. (in Chinese
ZHANG Chuwei. Study on the coupled calculation of combustion and heat transfer in LOX/methane rocket engine[D]. Beijing: China Aerospace Science and Technology Corporation, 2017. (in Chinese)
|
| [24] |
尹亮,刘伟强. 液氧/甲烷发动机研究进展与技术展望[J]. 航空兵器,2018,25(4): 21-27. YIN Liang,LIU Weiqiang. Review and prospect of LOX/methane rocket engine systems[J]. Aero Weaponry,2018,25(4): 21-27. (in Chinese
|
| [25] |
TANATSUGU N,SATO T,BALEPIN V,et al. Development study on ATREX engine: AIAA-96-4553 [R]. Norfolk,USA: AIAA,2003.
|
| [26] |
HARADA K,TANATSUGU N,SATO T. Development study on pre-cooler for ATREX engine: AIAA-99-4897 [R]. Norfolk,USA: AIAA,1999.
|
DownLoad:
