| Citation: | WANG Ziwen, LIU Haiyong, LIU Cunliang, et al. Study on cooling effectiveness and flow resistance characteristics of a double-layer corrugated heat shield with variable phase differences[J]. Journal of Aerospace Power, 2025, 40(5):20230600 doi: 10.13224/j.cnki.jasp.20230600 |
In order to solve the problem of large amount of cold air and local low cooling effectiveness area caused by the characteristic of corrugated structure in the longitudinal corrugated heat shield of an afterburner, a double-layer corrugated heat shield cooling structure was proposed. The cooling effectiveness and flow resistance characteristics of the double-layer corrugated heat shield with varying phase difference and amplitude ratio were studied by numerical simulation. The results showed that when the phase difference was from −π/4 to π/4, the local low cooling effectiveness area was improved, and the surface average overall cooling effectiveness and the temperature uniformity of the heat shield were improved at the same time. The relative surface average overall cooling effectiveness and cooling effectiveness uniformity of the double-layer corrugated heat shield with phase difference π/8 were the highest, i.e. 10.49% and 13.44%, respectively. When the phase difference was too large in the positive and negative directions, it may lead to the unreasonable flow rate distribution of the film holes and could increase the shrinkage loss of the film holes entrance. In addition, it was found that the increase of amplitude ratio can effectively improve the cooling effectiveness near the peak of wave and reduce the cooling effectiveness difference between the peak and the valley of the longitudinal corrugated effusion plate. When the amplitude ratio was 2, the cooling effect was the best.
| [1] |
李享. 加力燃烧室振荡燃烧的影响因素与抑制技术研究[D]. 南京: 南京航空航天大学,2016. LI Xiang. Research on influence factors and suppression techniques of oscillation combustion in afterburner[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2016. (in Chinese
LI Xiang. Research on influence factors and suppression techniques of oscillation combustion in afterburner[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016. (in Chinese)
|
| [2] |
张孝春,孙雨超,刘涛. 先进加力燃烧室设计技术综述[J]. 航空发动机,2014,40(2): 24-30,60. ZHANG Xiaochun,SUN Yuchao,LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine,2014,40(2): 24-30,60. (in Chinese
ZHANG Xiaochun, SUN Yuchao, LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine, 2014, 40(2): 24-30, 60. (in Chinese)
|
| [3] |
FUNAZAKI K,IGARASHI T,KOIDE Y,et al. Studies on cooling air ejected over a corrugated wall: its aerodynamic behavior and film effectiveness: ASME Paper 2001-GT-0143[R]. New Orleans,US: ASME,2001.
|
| [4] |
QU Lihong,ZHANG Jingzhou,TAN Xiaoming,et al. Numerical investigation on adiabatic film cooling effectiveness and heat transfer coefficient for effusion cooling over a transverse corrugated surface[J]. Chinese Journal of Aeronautics,2017,30(2): 677-684. doi: 10.1016/j.cja.2017.02.012
|
| [5] |
SINGH K,PREMACHANDRAN B,RAVI M R. Numerical investigation of film cooling on a 2D corrugated surface[J]. Numerical Heat Transfer: Part A Applications,2016,70(11): 1253-1270. doi: 10.1080/10407782.2016.1230431
|
| [6] |
SINGH K,PREMACHANDRAN B,RAVI M R. Experimental and numerical studies on film cooling of a corrugated surface[J]. Applied Thermal Engineering,2016,108: 312-329. doi: 10.1016/j.applthermaleng.2016.07.093
|
| [7] |
SINGH K,PREMACHANDRAN B,RAVI M R. Effect of thermal barrier coating and gas radiation on film cooling of a corrugated surface[J]. Journal of Heat Transfer,2018,140(9): 094504. doi: 10.1115/1.4039761
|
| [8] |
REN Haoliang,LIU Youhong,DU Liwei. An experimental study of flow and heat transfer performance of a longitudinal corrugated liner for a combustion chamber[J]. Applied Thermal Engineering,2017,127: 1305-1316. doi: 10.1016/j.applthermaleng.2017.08.137
|
| [9] |
唐婵,常海萍. 发散孔纵向波纹隔热屏气膜冷却特性[J]. 航空动力学报,2009,24(1): 18-24. TANG Chan,CHANG Haiping. Numerical simulation of effusion holes on the longitudinal ripple heat shield[J]. Journal of Aerospace Power,2009,24(1): 18-24. (in Chinese
TANG Chan, CHANG Haiping. Numerical simulation of effusion holes on the longitudinal ripple heat shield[J]. Journal of Aerospace Power, 2009, 24(1): 18-24. (in Chinese)
|
| [10] |
唐婵,常海萍. 发散孔纵向波纹隔热屏气膜冷却特性研究[J]. 燃气轮机技术,2009,22(1): 37-41,60. TANG Chan,CHANG Haiping. Numerical simulation on air film cooling characters of the longitudinal ripple heat shield with effusion holes[J]. Gas Turbine Technology,2009,22(1): 37-41,60. (in Chinese doi: 10.3969/j.issn.1009-2889.2009.01.009
TANG Chan, CHANG Haiping. Numerical simulation on air film cooling characters of the longitudinal ripple heat shield with effusion holes[J]. Gas Turbine Technology, 2009, 22(1): 37-41, 60. (in Chinese) doi: 10.3969/j.issn.1009-2889.2009.01.009
|
| [11] |
刘友宏,任浩亮. 气膜孔倾角对层板隔热屏冷却性能影响[J]. 推进技术,2016,37(2): 281-288. LIU Youhong,REN Haoliang. Effects of film cooling hole angles of inclination on cooling performance of lamilloy heat shield[J]. Journal of Propulsion Technology,2016,37(2): 281-288. (in Chinese
LIU Youhong, REN Haoliang. Effects of film cooling hole angles of inclination on cooling performance of lamilloy heat shield[J]. Journal of Propulsion Technology, 2016, 37(2): 281-288. (in Chinese)
|
| [12] |
刘友宏,李英,杨旭. 冲击/发散冷却层板隔热屏冷却性能及对比[J]. 航空动力学报,2014,29(6): 1272-1278. LIU Youhong,LI Ying,YANG Xu. Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield[J]. Journal of Aerospace Power,2014,29(6): 1272-1278. (in Chinese
LIU Youhong, LI Ying, YANG Xu. Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield[J]. Journal of Aerospace Power, 2014, 29(6): 1272-1278. (in Chinese)
|
| [13] |
刘友宏,陈超,任浩亮. 堵塞比对波纹板隔热屏冷却性能的影响[J]. 科学技术与工程,2018,18(4): 169-174. LIU Youhong,CHEN Chao,REN Haoliang. Effects of blockage ratio on cooling characteristics of wave heat shield[J]. Science Technology and Engineering,2018,18(4): 169-174. (in Chinese doi: 10.3969/j.issn.1671-1815.2018.04.027
LIU Youhong, CHEN Chao, REN Haoliang. Effects of blockage ratio on cooling characteristics of wave heat shield[J]. Science Technology and Engineering, 2018, 18(4): 169-174. (in Chinese) doi: 10.3969/j.issn.1671-1815.2018.04.027
|
| [14] |
LIU Yuyang,RAO Yu,YANG Li,et al. Flow and heat transfer characteristics of double-wall cooling with multi-row short film cooling hole arrangements[J]. International Journal of Thermal Sciences,2021,165: 106878. doi: 10.1016/j.ijthermalsci.2021.106878
|
| [15] |
许全宏,林宇震,刘高恩. 冲击/发散复合冷却方式发散壁换热系数研究[J]. 航空动力学报,2004,19(2): 213-218. XU Quanhong,LIN Yuzhen,LIU Gaoen. Study of the effusion wall film heat transfer coefficients of impingement/effusion double wall cooling method[J]. Journal of Aerospace Power,2004,19(2): 213-218. (in Chinese doi: 10.3969/j.issn.1000-8055.2004.02.009
XU Quanhong, LIN Yuzhen, LIU Gaoen. Study of the effusion wall film heat transfer coefficients of impingement/effusion double wall cooling method[J]. Journal of Aerospace Power, 2004, 19(2): 213-218. (in Chinese) doi: 10.3969/j.issn.1000-8055.2004.02.009
|
| [16] |
许全宏,林宇震,刘高恩. 冲击加多斜孔双层壁冷却方式冲击换热系数[J]. 大连理工大学学报,2001,41(增刊1): 63-66. XU Quanhong,LIN Yuzhen,LIU Gaoen. Heat transfer coefficient of impingement/effusion double wall cooling method[J]. Journal of Dalian University of Technology,2001,41(Suppl.1): 63-66. (in Chinese
XU Quanhong, LIN Yuzhen, LIU Gaoen. Heat transfer coefficient of impingement/effusion double wall cooling method[J]. Journal of Dalian University of Technology, 2001, 41(Suppl.1): 63-66. (in Chinese)
|
| [17] |
许全宏,林宇震,刘高恩. 冲击加多斜孔双层壁冷却方式流量系数研究[J]. 推进技术,2000,21(5): 49-52. XU Quanhong,LIN Yuzhen,LIU Gaoen. Discharge coefficient of double wall with discrete hole and inclined multihole for combustor liner[J]. Journal of Propulsion Technology,2000,21(5): 49-52. (in Chinese doi: 10.3321/j.issn:1001-4055.2000.05.014
XU Quanhong, LIN Yuzhen, LIU Gaoen. Discharge coefficient of double wall with discrete hole and inclined multihole for combustor liner[J]. Journal of Propulsion Technology, 2000, 21(5): 49-52. (in Chinese) doi: 10.3321/j.issn:1001-4055.2000.05.014
|
| [18] |
NIU Jiajia,LIU Cunliang,LIU Haiyong,et al. Theoretical and experimental analysis of overall cooling effectiveness for afterburner double-wall heat shield[J]. International Journal of Heat and Mass Transfer,2021,176: 121360. doi: 10.1016/j.ijheatmasstransfer.2021.121360
|
| [19] |
NIU Jiajia,LIU Cunliang,FU Song,et al. Experiment investigation of impingement/effusion cooling on overall cooling effectiveness and temperature gradients of afterburner heat shields in a high-performance aircraft engine[J]. Experimental Thermal and Fluid Science,2022,139: 110698. doi: 10.1016/j.expthermflusci.2022.110698
|
| [20] |
刘海涌,牛嘉嘉,刘存良,等. 开孔率对加力燃烧室隔热屏冷却特性的影响[J]. 航空发动机,2022,48(6): 64-70. LIU Haiyong,NIU Jiajia,LIU Cunliang,et al. Influence of open area on cooling characteristics of afterburner liner[J]. Aeroengine,2022,48(6): 64-70. (in Chinese
LIU Haiyong, NIU Jiajia, LIU Cunliang, et al. Influence of open area on cooling characteristics of afterburner liner[J]. Aeroengine, 2022, 48(6): 64-70. (in Chinese)
|
| [21] |
雷庆春,张鑫鑫. 一种采用波纹型隔板的双层壁防振隔热屏: CN116221775A[P]. 2023-06-06.
|
| [22] |
朱惠人,徐志鹏,张丽,等. 一种双层壁冷却装置及应用: CN114812257A[P]. 2022-07-29.
|
| [23] |
郭涛,谢龙,刘存良,等. 用于矢量喷管的具有横向波纹冲击孔板的双层壁冷却结构: CN109882314B[P]. 2021-09-10.
|