基于射流管延伸和声激励器集成的受限横流通道方阵射流冲击传热强化

吕元伟; 谭钧文; 毛佳宁; 陈格; 张镜洋; 张靖周; 王奉明

doi:10.7527/S1000-6893.2026.33064

航空学报 >

0 1 - 0

DOI: https://doi.org/10.7527/S1000-6893.2026.33064

基于射流管延伸和声激励器集成的受限横流通道方阵射流冲击传热强化

吕元伟 ,
谭钧文 ,
毛佳宁 ,
陈格 ,
张镜洋 ,
张靖周 ,
王奉明

展开

1. 南京航空航天大学
2. 上海卫星工程研究所
3. 南京航空航天大学航天学院
4. 南京航空航天大学能源与动力学院
5. 空军装备研究院总体所（中国科学院热物所读博士）

收稿日期: 2025-11-10

修回日期: 2026-05-12

网络出版日期: 2026-05-14

基金资助

国家自然科学基金;中国航发集团产学研合作项目基金

收起

On Heat Transfer Enhancement of Square-Array Jet Impingement in a Confined Crossflow Channel by Using Extended Jet Pipe and Integrated Acoustic Actuator

TAN Jun-Wen ,
MAO Jia-Ning ,
CHEN Ge ,
ZHANG Jing-Yang ,
ZHANG Jing-Zhou ,
WANG Feng-Ming

Expand

Received date: 2025-11-10

Revised date: 2026-05-12

Online published: 2026-05-14

Supported by

National Natural Science Foundation of China;Industry-University-Research Fund of Aero Engine Corporation of China

Fold

摘要

针对无量纲高度H/d=3的受限横流通道中的2′2方阵连续射流(无量纲节距X/d=Y/d=4)冲击对流传热开展了试验研究，重点关注方阵中央声激励合成射流集成和射流管延伸的主被动强化及其组合方式传热强化效果。方阵射流雷诺数Re=3000~10000，在f=250Hz恒定激励频率下，相应的合成射流与方阵射流速度比RSJ-CJ=2.0~0.6；射流管延伸调节喷口与壁面的无量纲法向距离为L/d=1~3。在本文参数范围内，研究结果表明：Re=3000时，合成射流集成方式的传热强化效果明显高于射流管延伸方式，在组合方式的对流传热强化中占据主导机制，与无合成射流集成和无射流管延伸的基准情形相比，当横流与方阵射流速度比RCF-CJ?0.67时区域面积平均努塞尔数(Nus-av)相对提高可达2倍以上；而在Re=10000时，射流管延伸则为对流传热强化的主导机制，RCF-CJ=0.5下的Nus-av相对基准情形提升幅值可达1倍，此时在射流管延伸方阵中合成射流集成的作用几乎得不到体现；方阵射流管延伸和合成射流集成的组合方式只有当两者强化传热作用基本相当时方能体现出其有益性，相对于单一方式，组合方式在Re=5000和RCF-CJ=0.6~0.8时显现出较为显著的强化传热再提升效果。

关键词： 受限横流通道; 方阵连续射流; 声激励器; 合成射流; 射流管延伸; 对流传热强化

本文引用格式

吕元伟 , 谭钧文 , 毛佳宁 , 陈格 , 张镜洋 , 张靖周 , 王奉明 . 基于射流管延伸和声激励器集成的受限横流通道方阵射流冲击传热强化[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2026.33064

Abstract

An experimental investigation is performed to the convective heat transfer in a confined crossflow channel with a specific dimension-less height of H/d=3, produced from a 2′2 square-array impinging jets with dimensionless pitches of X/d=Y/d=4. Particular focus is played on the heat transfer enhancement by using the passively extended jet pipes and the actively center-positioned synthetic jet in the continuous-jet square array, as well as their combination schemes. In the present study, square-array jet Reynolds number (Re)ranges from 3000~10000, and the synthetic jet acoustic actuator is driven at a fixed frequency of f=100Hz. Correspondingly, the synthetic jet velocity ratios (defined as the ratio of synthetic jet characteristic velocity to square-array jet ejecting velocity, RSJ-CJ)are varied from 2.0 (under Re=3000)to 0.6 (under Re=10000). From the jet pipe extension, the dimensionless normal distance between jet outlet and targeting wall is adjusted in a range of L/d=1~3. Within the scope of this study, the heat transfer enhancement roles are clearly illustrated. Under Re=3000, the synthetic jet integration demonstrates a significantly stronger heat transfer augment role than the jet pipe extension, taking on dominant heat transfer enhancement mechanism in the combination scheme. With respect to the base-line situation (no synthetic jet integration and no jet pipe extension), the area-averaged Nusselt number on a specified zone could be increased up to 200% when the crossflow velocity ratio (defined as the ratio of crossflow inlet velocity to square-array jet ejecting velocity, RCF-CJ)beyond 0.67. Whereas under Re=10000, the jet pipe extension plays dominant heat transfer enhancement mechanism on the otherwise. the area-averaged Nusselt number could be increased up to 100% at RCF-CJ=0.5 in relation to the baseline situation. Meanwhile, in the square array with the extended jet pipes, the role of synthetic jet integration is very faint. The most possibilities wherein the combination of synthetic jet integration and jet pipe extension could exhibit obviously its significance on heat transfer enhancement appear when both schemes display equivalent heat transfer augment roles. For instance, under Re=5000 and RCF-CJ=0.6~0.8, the combination scheme shows an obviously further improvement on heat transfer enhancement, in related to the single scheme either in active or passive.

Key words： Confined crossflow channel; Square-array continuous jets; Acoustic actuator; Synthetic jet; Extended jet pipe; Convective heat trans-fer enhancement

参考文献

[1] VISKANTA R. Heat transfer to impinging isothermal gas and flame jets [J]. Experimental Thermal and Fluid Sci-ence, 1993, 6: 111–134.
[2] ALI C, GEORG K, BIRGIT G. Review of jet impinge-ment heat and mass transfer for industrial application [J]. Heat Transfer Research, 2021, 52: 61–91.
[3] 刘宇阳, 代欣波, 王强, 等．热气冲击射流换热特性与防冰效果研究[J]. 航空学报, 2026, 47(6): 632653.
LIU Y Y, DAI X B, WANG Q, et al. Study on heat transfer characteristics and anti-icing performance of hot-air impingement jets [J]. Acta Aeronautica et Astro-nautica Sinica, 2026, 47(6): 632653 (in Chinese).
[4] CARLOMAGNO G M, IANIRO A. Thermo-fluid-dynamics of submerged jets impinging at short nozzle-to-plate distance: A review [J]. Experimental Thermal and Fluid Science, 2014, 58: 15–35.
[5] EKKAD S V, SINGH P. A modern review on jet im-pingement heat transfer methods [J]. ASME Journal of Heat Transfer, 2021, 143: 064001.
[6] KARAGOZIAN A R. The jet in crossflow [J]. Physics of Fluids, 2014, 26(10): 101303.
[7] GOLDSTEIN R J, BEHBAHANI A I. Impingement of a circular jet with and without cross flow [J]. Interna-tional Journal of Heat and Mass Transfer, 1982, 25(9): 1377–1382.
[8] WANG L, SUNDEN B, BORG A, et al. Heat transfer characteristics of an impinging jet in crossflow [J]. ASME Journal of Heat Transfer, 2011, 133: 122202.
[9] WANG P F, LIU J, WANG P, et al. Effect of internal crossflow on impingement cooling flow and heat trans-fer characteristics [J]. International Communications in Heat and Mass Transfer, 2024, 159: 108119.
[10] CHAMBERS A C, GILLSPIE D R H, IRELAND P T, et al. Enhancement of impingement cooling in a high cross flow channel using shaped impingement cooling holes [J]. ASME Journal of Turbomachinery, 2010, 132: 021001.
[11] CHI Z R, KAN R, REN J, et al. Experimental and nu-merical study of the anti-cross flows impingement cooling structure [J]. International Journal of Heat and Mass Transfer, 2013, 64: 567–580.
[12] YU Y Z, ZHANG J Z, SHAN Y. Convective heat trans-fer of a row of air jets impingement excited by triangu-lar tabs in a confined crossflow channel [J]. Interna-tional Journal of Heat and Mass Transfer, 2015, 80: 126–138.
[13] RIZK M G, KAOUD O G, ELDIN HUSSIN A M T A, et al. Analysis of transport phenomena on cooling a flat surface using swirl jet impingement with crossflow [J]. International Journal of Thermal Sciences, 2023, 194(1): 108537.
[14] WANG C L, LUO L, WANG L, et al. Effects of vortex generators on the jet impingement heat transfer in cross-flow at different Reynolds numbers [J]. Interna-tional Journal of Heat and Mass Transfer, 2016, 96: 278–286.
[15] HE J, DENG Q, XIAO K, et al. Heat transfer enhance-ment of impingement cooling by different crossflow diverters [J]. ASME Journal of Heat Transfer, 2022, 144: 042001.
[16] CHEN L L, WEIGAND B, YANG H Q, et al. Numeri-cal heat transfer investigation of a single impingement jet with combined V-ribs and preliminary optimization of V-rib configuration in initial crossflow [J]. Interna-tional Journal of Thermal Sciences, 2024, 197: 108799.
[17] CATTAFESTA L N, SHEPLAK M. Actuators for active flow control [J]. Annual Review of Fluid Mechanics, 2011, 43: 247–272.
[18] 吕元伟, 张靖周, 唐婵, 等. 脉冲射流冲击平直表面的对流换热实验[J]. 航空学报, 2018, 39(4): 121695.
LYU Y W, ZHANG J Z, TANG C, et al. Experiment of convective heat transfer of pulsed jet impingement on a flat surface [J]. Acta Aeronautica et Astronautica Sinca, 2018, 39(4): 121695.
[19] MAGHRABIE H M. Heat transfer intensification of jet impingement using exciting jets-A comprehensive re-view [J]. Renewable and Sustainable Energy Reviews, 2021, 139: 110684.
[20] SALIBA G C, BATIKH A, COLIN S, et al. Pulsed impinging jets for heat transfer: a short review [J]. ASME Journal of Heat and Mass Transfer, 2023, 145: 110801.
[21] SMITH B L, GLEZER A. The formation and evolution of synthetic jets [J]. Physics of Fluids, 1998, 10: 2281–2297.
[22] TANG H, SALUNKHE P, ZHENG Y Y, et al. On the use of synthetic jet actuator arrays for active flow sepa-ration control [J]. Experimental Thermal and Fluid Sci-ence, 2014, 57: 1–10.
[23] WALIMBE P, AGRAWAL A, CHAUDHARI M. Flow characteristics and novel applications of synthetic jets: A review [J]. ASME Journal of Heat Transfer, 2021, 143: 112301.
[24] 陆逸然, 王晋军. 高效合成射流激励器研究进展及展望[J]. 力学进展, 2024, 54(1): 61–85.
LU Y R, WANG J J. Review and prospect on the efficient synthetic jet [J]. Advances in Mechanics, 2024, 54(1): 61–85 (in Chinese).
[25] 罗振兵, 王浩, 赵志杰. 合成双射流理论及其赋能航空技术进展[J]. 航空学报, 2025, 46(5): 531821.
LUO Z B, WANG H, ZHAO Z J. Theory of dual synthetic jets and its empowerment of advancements in aeronautical technology [J]. Acta Aeronautica et Astro-nautica Sinica, 2025, 46(5): 531821 (in Chinese).
[26] KRISHAN G, AW K C, SHARMA R N. Synthetic jet impingement heat transfer enhancement - A review [J]. Applied Thermal Engineering, 2019, 149: 1305–1323.
[27] ARSHAD A, JABBAL M, Yan Y Y. Synthetic jet actua-tors for heat transfer enhancement - A critical review [J]. International Journal of Heat and Mass Transfer, 2020, 146: 118815.
[28] TIMCHENKO V, REIZES J, LEONARDI E. An eval-uation of synthetic jets for heat transfer enhancement in air cooled micro-channels [J]. International Journal of Numerical Methods for Heat and Fluid Flow, 2007, 17: 263–283.
[29] TRAVNICEK Z, TESAR V, BROUCKOVA Z, et al. Annular impinging jet controlled by radial synthetic jets [J]. Heat Transfer Engineering, 2014, 35: 1450–1461.
[30] IWANA T, SUENAGA K, SHIRAI K, et al. Heat trans-fer and fluid flow characteristics of impinging jet using combined device with triangular tabs and synthetic jets [J]. Experimental Thermal and Fluid Science, 2015, 68: 322–329.
[31] TAN J W, ZHANG J Z, LYU Y W, et al. Experimental study on convective heat transfer of hybrid impinge-ment configuration by square-array continuous jets and a center-positioned synthetic jet [J]. International Jour-nal of Heat and Mass Transfer, 2023, 215: 124414.
[32] TAN J W, SUN W J, LYU Y W, et al. Convective heat transfer improvement for a single row of continuous air jets by the acoustic-actuator integration [J]. Internation-al Journal of Thermal Sciences, 2024, 203: 109122.
[33] SMITH B L, SWIFT G W. A comparison between syn-thetic jets and continuous jets [J]. Experiments in Flu-ids, 2003, 34: 467–472.
[34] TAN X M, ZHANG J Z, SHAN Y, et al. An experi-mental investigation on comparison of synthetic and continuous jets impingement heat transfer [J]. Interna-tional Journal of Heat and Mass Transfer, 2015, 90: 227–238.
[35] LYU Y W, TAN J W, ZHANG J Z, et al. Active heat transfer enhancement roles by an acoustic actuator inte-gration into square array of continuous jets in the pres-ence of crossflow [J]. International Journal of Heat and Mass Transfer, 2025, 240: 126568.
[36] GIL P, STRZELCZYK P. Performance and efficiency of loudspeaker driven synthetic jet actuator [J]. Experi-mental Thermal Fluid and Science, 2016, 76: 163–174.
[37] 谭钧文, 吕元伟, 张靖周, 等. 喷口直径对声激励器输入功率和膜片振动以及合成射流冲击传热的综合影响[J]. 中国科学: 技术科学, 2024, 54: 2347–2362.
TAN J W, LYU Y W, ZHANG JZ, et al. Comprehen-sive effects of orifice diameter on input power and dia-gram vibration of acoustic actuator as well as flow and heat transfer characteristics of synthetic jet [J]. Scientia Sinica (Technologica), 2024, 54: 2347–2362 (in Chi-nese).
[38] GRECO C S, PAOLILLO G, IANIRO A, et al. Effects of the stroke length and nozzle-to-plate distance on synthetic jet impingement heat transfer [J]. International Journal of Heat and Mass Transfer, 2018, 117: 1019–1031.
[39] MOFFAT R J. Describing the uncertainties in experi-mental results [J]. Experimental Thermal and Fluid Sci-ence, 1988, 1: 3–17.
[40] FLORSCHUETZ L W, TRUMAN C R, METZGER D E. Streamwise flow and heat transfer distributions for jet array impingement with crossflow [J]. ASME Jour-nal of Heat Transfer, 1981, 103: 337–342.

Options

文章导航

模态框（Modal）标题

摘要

本文引用格式

Abstract

参考文献