PDF下载 分享
[1]张 萌,孙 冰.人工粗糙度对矩形弯曲管道流动与传热数值模拟[J].火箭推进,2020,46(01):20-27.
 ZHANG Meng,SUN Bing.Numerical simulation of flow and heat transfer in a curved rectangular channel with artificial roughness[J].Journal of Rocket Propulsion,2020,46(01):20-27.
点击复制

人工粗糙度对矩形弯曲管道流动与传热数值模拟

参考文献/References:

[1] 刘国斌.液体火箭发动机原理[M].北京:宇航出版社,1993.
[2] 蔡国飙.液体火箭发动机设计[M].北京:北京航空航天大学出版社, 2011.
[3] 章思龙, 秦江, 周伟星, 等.高超声速推进再生冷却研究综述[J].推进技术, 2018, 39(10):2177-2190.
[4] 陈建华, 杨宝庆, 周立新, 等.人为粗糙度强化换热机理分析及效果评估[J].火箭推进, 2004, 30(4):1-5.CHEN J H, YANG B Q, ZHOU L X, et al.The mechanism and effect of artificial roughness on heat transfer enhancement[J].Journal of Rocket Propulsion, 2004, 30(4):1-5.
[5] HOSSAIN J, TRAN L V, CARPENTER C, et al.Numerical study of enhancement of regenerative cooling using ribs[R]. AIAA 2013-3996.
[6] XU K K, TANG L J, MENG H.Numerical study of supercritical-pressure fluid flows and heat transfer of methane in ribbed cooling tubes[J].International Journal of Heat and Mass Transfer, 2015, 84:346-358.
[7] KAMALI R, BINESH A R.The importance of rib shape effects on the local heat transfer and flow friction characteristics of square ducts with ribbed internal surfaces[J].International Communications in Heat and Mass Transfer, 2008, 35(8):1032-1040.
[8] NARAGHI M, DASSONVILLE R.Improved correlations for curvature effects in cooling channels of rocket engines[C]//48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Atlanta, Georgia.Reston, Virigina:AIAA, 2012.
[9] VALENTIN J, NARAGHI M.Effects cooling channel curvature on coolant secondary flow and heat transfer[C]//46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Nashville, TN.Reston, Virigina:AIAA, 2010.
[10] PIZZARELLI M.Effectiveness of spalart-allmaras turbulence model in analysis of curved cooling channels[J].AIAA Journal, 2013, 51(9):2158-2167.
[11] PIZZARELLI M, NASUTI F, ONOFRI M.CFD analysis of curved cooling channel flow and heat transfer in rocket engines[C]//46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Nashville, TN.Reston, Virigina:AIAA, 2010.
[12] 康玉东, 孙冰.燃气非平衡流再生冷却流动传热数值模拟[J].推进技术, 2011, 32(1):119-124.
[13] 丁珏, 翁培奋.三种湍流模式数值模拟直角弯管内三维分离流动的比较[J].计算物理, 2003, 20(5):386-390.
[14] 赵金辉, 王志国, 晋世强.不同曲率直径比下90°弯管内部流场分析[J].轻工科技, 2014, 30(8):64-65.
[15] 孙业志, 胡寿根, 赵军, 等.不同雷诺数下90°弯管内流动特性的数值研究[J].上海理工大学学报, 2010, 32(6):525-529.
[16] 湛含辉, 朱辉, 陈津端, 等.90°弯管内二次流(迪恩涡)的数值模拟[J].锅炉技术, 2010, 41(4):1-5.

相似文献/References:

[1]孙 鑫,杨成虎.5 kN再生冷却发动机推力室传热研究[J].火箭推进,2012,38(02):32.
 SUN Xin,YANG Cheng-hu.Heat transfer investigation for 5 kN regeneratively-cooled engine thrust chamber[J].Journal of Rocket Propulsion,2012,38(01):32.
[2]徐辉,易琪,钟徐,等.1 0kN双向摇摆再生冷却发动机技术研究[J].火箭推进,2009,35(05):8.
 Xu Hui,Yi Qi,Zhong Xu,et al.Research on 1 0kN gimbaled regeneratively cooled engine[J].Journal of Rocket Propulsion,2009,35(01):8.
[3]方磊.刘伟.姿控用再生冷却推力室传热特性研究[J].火箭推进,2008,34(06):6.
 Fang Lei,Liu Wei.Research on heat transf.er characteristic of regeneratiVely cooled attitude control engine thmst chamber[J].Journal of Rocket Propulsion,2008,34(01):6.
[4]栾叶君,孙纪国,田昌义,等.氢氧推力室再生冷却内壁故障分析[J].火箭推进,2006,32(05):17.
 Luan Yejun,Sun Jiguo,Tian Changyi,et al.Failure analysis on regeneratively cooled wall of a hydrogen-oxygen thrust chamber[J].Journal of Rocket Propulsion,2006,32(01):17.
[5]徐辉,林庆国,汪允武,等.挤压式低室压推力室再生冷却问题[J].火箭推进,2006,32(06):12.
 Xu Hui,Lin Qingguo,Wang Yunwu,et al.Regenerative cooling of the pressure-fed thruster with low-pressure chamber[J].Journal of Rocket Propulsion,2006,32(01):12.
[6]许晓勇,赵世红,王召.轻质钛合金喷管在氢氧发动机上的应用研究[J].火箭推进,2016,42(04):1.
 XU Xiaoyong,ZHAO Shihong,WANG Zhao.Application of lightweight titanium alloy nozzle in LOX-LH2 rocket engine[J].Journal of Rocket Propulsion,2016,42(01):1.
[7]金烜,沈赤兵,吴先宇,等.超燃冲压发动机再生冷却技术研究进展[J].火箭推进,2016,42(05):66.[doi:10.3969/j.issn.1672-9374.2016.05.012]
 JIN Xuan,SHEN Chibing,WU Xianyu,et al.Progress of regenerative cooling technology for scramjet[J].Journal of Rocket Propulsion,2016,42(01):66.[doi:10.3969/j.issn.1672-9374.2016.05.012]
[8]刘朝晖,陈雪娇,蒋榕培.超高参数火箭煤油在小通道圆管内的流动换热特性[J].火箭推进,2024,50(05):114.[doi:10.3969/j.issn.1672-9374.2024.05.011]
 LIU Zhaohui,CHEN Xuejiao,JIANG Rongpei.Convective heat transfer characteristics of rocket kerosene in circular mini-tubes at ultra-high parameter conditions[J].Journal of Rocket Propulsion,2024,50(01):114.[doi:10.3969/j.issn.1672-9374.2024.05.011]
[9]张 萌,孙 冰.液氧/甲烷发动机推力室肋强化换热技术数值研究[J].火箭推进,2021,47(02):19.
 ZHANG Meng,SUN Bing.Numerical study on enhanced heat transfer technology ofLOX/CH4engine chamber with ribs[J].Journal of Rocket Propulsion,2021,47(01):19.

备注/Memo

收稿日期:2019-04-13; 修回日期:2019-05-24基金项目:国家自然科学基金(11602186)作者简介:张萌(1993—),男,博士,研究领域为液体火箭发动机热防护仿真

更新日期/Last Update: 2020-02-25