| Citation: | CHENG Jingli, HUANG Sheng, ZHOU Li, et al. Investigation on influence mechanism of exit aspect ratio on thermal-solid interaction response of serpentine nozzle[J]. Journal of Aerospace Power, 2025, 40(2):20230228 doi: 10.13224/j.cnki.jasp.20230228 |
In order to clarify the effect of exit aspect ratio on the flow heat transfer and structural response of serpentine nozzle, a serial two-way loose coupling method based on computational structural dynamics/computational fluid dynamics (CSD/CFD) was used to study the effect of thermal-solid coupling response at different aspect ratios. Results were obtained as follows: the overall heatflux distribution of the nozzle under the action of the bending configuration was not uniform, with large variability at each location, while the heatflux distribution of individual nozzles was similar; the heatflux increased continuously at the second bend as exit aspect ratio increased; the vortex structure was generated at the exit isometric section, and the presence of the vortex structure hindered the heat transfer; in structural response, the distribution of stress in each serpentine nozzle was similar, but the maximum stress existed in two locations, including the nozzle exit end and the upper wall of the second bend channel. As the exit aspect ratio rose, the maximum stress also rose, and appeared in advance. Maximum stress with aspect ratio of 10 increased by 28% compared with the minimum stress, and the moment of appearance was 23.84 s earlier.
| [1] |
陈利玲,蔡亚梅. 国外防空防天装备发展现状与趋势[J]. 航天电子对抗,2010,26(3): 5-8. CHEN Liling,CAI Yamei. Present and future of foreign air and space defense equipment[J]. Aerospace Electronic Warfare,2010,26(3): 5-8. (in Chinese doi: 10.3969/j.issn.1673-2421.2010.03.002
CHEN Liling, CAI Yamei. Present and future of foreign air and space defense equipment[J]. Aerospace Electronic Warfare, 2010, 26(3): 5-8. (in Chinese) doi: 10.3969/j.issn.1673-2421.2010.03.002
|
| [2] |
罗沛,郑敏. 航空发动机尾喷管热流固耦合分析[J]. 国际航空航天科学,2016,4(4): 85-96. LUO Pei,ZHENG Min. Thermal-fluid-solid coupling analysis of aero-engine nozzle[J]. Journal of Aerospace Science and Technology,2016,4(4): 85-95.
LUO Pei, ZHENG Min. Thermal-fluid-solid coupling analysis of aero-engine nozzle[J]. Journal of Aerospace Science and Technology, 2016, 4(4): 85-95.
|
| [3] |
CROWE D S,MARTIN C L. Effect of geometry on exit temperature from serpentine exhaust nozzles: AIAA-2015-1670[R]. Reston,US: AIAA,2015.
|
| [4] |
DEATON J,GRANDHI R. Thermal-structural analysis of engine exhaust-washed structures: AIAA-2010-9236[R]. Reston,US: AIAA,2010.
|
| [5] |
DEATON J,GRANDHI R. Thermal-structural design and optimization of engine exhaust-washed structures: AIAA-2011-1903 [R]. Reston,US: AIAA,2011.
|
| [6] |
URBANCZYK P S,ALONSO J J,NIGAM N,et al. Coupled multiphysics analysis for design of advanced exhaust systems: AIAA-2017-0799 [R]. Reston,US: AIAA,2017.
|
| [7] |
DALENBRING M,SMITH J. Simulation of S-duct dynamics using fluid-structure coupled CFD: AIAA-2006-2981[R]. Reston,US: AIAA,2006.
|
| [8] |
孙鹏,周莉,王占学,等. 双S弯喷管的流固耦合特性研究[J]. 推进技术,2022,43(10): 158-167. SUN Peng,ZHOU Li,WANG Zhanxue,et al. Fluid-structure interaction characteristic of double serpentine nozzle[J]. Journal of Propulsion Technology,2022,43(10): 158-167. (in Chinese
SUN Peng, ZHOU Li, WANG Zhanxue, et al. Fluid-structure interaction characteristic of double serpentine nozzle[J]. Journal of Propulsion Technology, 2022, 43(10): 158-167. (in Chinese)
|
| [9] |
李秋琳,周莉,孙鹏,等. 出口宽高比对S弯喷管流固耦合特性影响[J]. 航空学报,2023,44(14): 628204. LI Qiulin,ZHOU Li,SUN Peng,et al. Influence mechanism of aspect ratio on fluid-structure interaction characteristics of serpentine nozzle[J]. Acta Aeronautica et Astronautica Sinica,2023,44(14): 628204. (in Chinese
LI Qiulin, ZHOU Li, SUN Peng, et al. Influence mechanism of aspect ratio on fluid-structure interaction characteristics of serpentine nozzle[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 628204. (in Chinese)
|
| [10] |
郭帅,徐惊雷,顾瑞. 单边膨胀喷管移动板的流固耦合研究[J]. 航空动力学报,2015,30(6): 1382-1390. GUO Shuai,XU Jinglei,GU Rui. Fluid-structure interaction study of slide tail plate of single expansion ramp nozzle[J]. Journal of Aerospace Power,2015,30(6): 1382-1390. (in Chinese
GUO Shuai, XU Jinglei, GU Rui. Fluid-structure interaction study of slide tail plate of single expansion ramp nozzle[J]. Journal of Aerospace Power, 2015, 30(6): 1382-1390. (in Chinese)
|
| [11] |
孙啸林. 低可探测S弯喷管设计及性能评估方法研究[D]. 西安: 西北工业大学,2018. SUN Xiaolin. Investigation on design method and performance estimation of low observable S-shaped nozzle[D]. Xi’an: Northwestern Polytechnical University,2018. (in Chinese
SUN Xiaolin. Investigation on design method and performance estimation of low observable S-shaped nozzle[D]. Xi’an: Northwestern Polytechnical University, 2018. (in Chinese)
|
| [12] |
孙鹏,周莉,王占学,等. 出口宽高比及旋流角对双涵道S弯喷管温度分布的影响[J]. 航空动力学报,2022,37(2): 391-403. SUN Peng,ZHOU Li,WANG Zhanxue,et al. Effect of aspect ratio and swirl angle on temperature distribution of double serpentine nozzle for turbofan[J]. Journal of Aerospace Power,2022,37(2): 391-403. (in Chinese
SUN Peng, ZHOU Li, WANG Zhanxue, et al. Effect of aspect ratio and swirl angle on temperature distribution of double serpentine nozzle for turbofan[J]. Journal of Aerospace Power, 2022, 37(2): 391-403. (in Chinese)
|
| [13] |
程稳. S弯喷管红外辐射特性预测及优化设计方法[D]. 西安: 西北工业大学,2019. CHENG Wen. Infrared signature prediction and optimization design method for serpentine nozzle[D]. Xi’an: Northwestern Polytechnical University,2019. (in Chinese
CHENG Wen. Infrared signature prediction and optimization design method for serpentine nozzle[D]. Xi’an: Northwestern Polytechnical University, 2019. (in Chinese)
|
| [14] |
JOPPICH W,KÜRSCHNER M. MpCCI: a tool for the simulation of coupled applications[J]. Concurrency and Computation Practice and Experience,2006,18: 183-192. doi: 10.1002/cpe.913
|
| [15] |
曹琪,李进贤,唐金兰,等. SRM点火瞬间流固耦合研究现状与发展探索[J]. 世界科技研究与发展,2009,31(5): 879-883,942. CAO Qi,LI Jinxian,TANG Jinlan,et al. Research actuality and development of coupling fluid-structure in SRM ignition transient[J]. World Sci-Tech R$D,2009,31(5): 879-883,942. (in Chinese doi: 10.3969/j.issn.1006-6055.2009.05.032
CAO Qi, LI Jinxian, TANG Jinlan, et al. Research actuality and development of coupling fluid-structure in SRM ignition transient[J]. World Sci-Tech R$D, 2009, 31(5): 879-883, 942. (in Chinese) doi: 10.3969/j.issn.1006-6055.2009.05.032
|
| [16] |
WIETING A,HOLDEN M. Experimental study of shock wave interference heating on a cylindrical leading edge at Mach 6 and 8[J]. AIAA Journal,1989,27(11): 1557-1565. doi: 10.2514/3.10301
|
| [17] |
DECHAUMPHAI P,THORNTON E A,WIETING A R. Flow-thermal-structural study of aerodynamically heated leading edges[J]. Journal of Spacecraft and Rockets,1989,26(4): 201-209. doi: 10.2514/3.26055
|
| [18] |
郭帅. 高超声速飞行器关键部件的多物理场耦合研究[D]. 南京: 南京航空航天大学,2016. GUO Shuai. Multidisciplinary study of key components in hypersonic flight vehicle[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2016. (in Chinese
GUO Shuai. Multidisciplinary study of key components in hypersonic flight vehicle[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016. (in Chinese)
|
| [19] |
黄杰. 高超声速飞行器流热固多物理场耦合计算研究[D]. 哈尔滨: 哈尔滨工业大学,2013. HUANG Jie. Study on hypersonic vehicle fluid-thermal-structure multi-physics coupling calculation[D]. Harbin: Harbin Institute of Technology,2013. (in Chinese
HUANG Jie. Study on hypersonic vehicle fluid-thermal-structure multi-physics coupling calculation[D]. Harbin: Harbin Institute of Technology, 2013. (in Chinese)
|
| [20] |
BILLIG F S. Shock-wave shapes around spherical-and cylindrical-nosed bodies[J]. Journal of Spacecraft and Rockets,1967,4(6): 822-823. doi: 10.2514/3.28969
|
| [21] |
ZOPE A D,SCHEMMEL A,BHATIA M,et al. Development and validation of fluid-thermal interaction solver for high fidelity transient simulations: AIAA-2020-3006 [R]. Reston,US: AIAA,2020.
|
| [22] |
KAMALI S,MAVRIPLIS D J,ANDERSON E M. Development and validation of a high-fidelity aero-thermo-elastic analysis capability: AIAA-2020-1449 [R]. Reston,US: AIAA,2020.
|
| [23] |
LEE C,BOEDICKER C. Subsonic diffuser design and performance for advanced fighter aircraft: AIAA-1985-3073 [R]. Reston,US: AIAA,1985.
|
| [24] |
孙啸林,王占学,周莉,等. 基于多参数耦合的S弯隐身喷管设计方法研究[J]. 工程热物理学报,2015,36(11): 2371-2375. SUN Xiaolin,WANG Zhanxue,ZHOU Li,et al. The design method of serpentine stealth nozzle based on coupled parameters[J]. Journal of Engineering Thermophysics,2015,36(11): 2371-2375. (in Chinese
SUN Xiaolin, WANG Zhanxue, ZHOU Li, et al. The design method of serpentine stealth nozzle based on coupled parameters[J]. Journal of Engineering Thermophysics, 2015, 36(11): 2371-2375. (in Chinese)
|