Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (24): 130290.doi: 10.7527/S1000-6893.2024.30290
• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles
Dingjin ZHANG, Juanmian LEI, Rui ZHAO(
)
Received:2024-02-18
Revised:2024-03-26
Accepted:2024-04-02
Online:2024-12-25
Published:2024-04-10
Contact:
Rui ZHAO
E-mail:zr8800@126.com
Supported by:CLC Number:
Dingjin ZHANG, Juanmian LEI, Rui ZHAO. Influence of wall temperature on receptivity of hypersonic flare cone boundary layer[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(24): 130290.
| 1 | ZHONG X L, WANG X W. Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers[J]. Annual Review of Fluid Mechanics, 2012, 44(1): 527-561. |
| 2 | 陈猛, 刘汝盟, 王立峰, 等. 国家自然科学基金新增代码 “航空航天力学”内涵及重要研究领域[J].航空学报, 2024, 45(2): 129947. |
| CHEN M, LIU R M, WANG L F, et al. Connotation and key research areas of new application code “Aerospace Mechanics” of the National Natural Science Foundation of China[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 129947 (in Chinese). | |
| 3 | 王宇天, 刘建新, 王晓坤, 等. 多孔壁面对高速边界层最优增长条带二次失稳的影响规律[J]. 航空学报, 2023, 44(22): 128519. |
| WANG Y T, LIU J X, WANG X K, et al. Effects of porous wall on secondary instability of optimal growth streaks in high speed boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 128519 (in Chinese). | |
| 4 | 周恒, 苏彩虹, 张永明. 超声速/高超声速边界层的转捩机理及预测[M]. 北京: 科学出版社, 2015. |
| ZHOU H, SU C H, ZHANG Y M. Transition mechanism and prediction of supersonic/hypersonic boundary layer[M]. Beijing: Science Press, 2015 (in Chinese). | |
| 5 | 孔维萱, 张辉, 阎超. 适用于高超声速边界层的转捩准则预测方法[J]. 导弹与航天运载技术, 2013(5): 54-58. |
| KONG W X, ZHANG H, YAN C. Transition criterion prediction method for hypersonic boundary layer[J]. Missiles and Space Vehicles, 2013(5): 54-58 (in Chinese). | |
| 6 | 周玲, 阎超, 郝子辉, 等. 转捩模式与转捩准则预测高超声速边界层流动[J]. 航空学报, 2016, 37(4): 1092-1102. |
| ZHOU L, YAN C, HAO Z H, et al. Transition model and transition criteria for hypersonic boundary layer flow[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(4): 1092-1102 (in Chinese). | |
| 7 | 符松, 王亮. 湍流转捩模式研究进展[J]. 力学进展, 2007, 37(3): 409-416. |
| FU S, WANG L. Progress in turbulence/transition modelling[J]. Advances in Mechanics, 2007, 37(3): 409-416 (in Chinese). | |
| 8 | 张雯, 刘沛清, 郭昊, 等. 湍流转捩工程预报方法研究进展综述[J]. 实验流体力学, 2014, 28(6): 1-12, 38. |
| ZHANG W, LIU P Q, GUO H, et al. Review of transition prediction methods[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(6): 1-12, 38 (in Chinese). | |
| 9 | 刘清扬,雷娟棉,刘周,等. 适用于可压缩流动的γ-Reθt -fRe 转捩模型[J]. 航空学报, 2022, 43(8): 125794. |
| LIU Q Y, LEI J M, LIU Z, et al. γ-Reθt -fRe transition model for compressible flow[J]. 2022, 43(8): 125794 (in Chinese). | |
| 10 | 苏彩虹. 高超声速边界层转捩预测中的关键科学问题: 感受性、扰动演化及转捩判据研究进展[J]. 空气动力学学报, 2020, 38(2): 355-367. |
| SU C H. Progress in key scientific problems of hypersonic bounary-layer transition prediction: receptivity, evolution of disturbances and transition criterion[J]. Acta Aerodynamica Sinica, 2020, 38(2): 355-367 (in Chinese). | |
| 11 | 罗纪生. 高超声速边界层的转捩及预测[J]. 航空学报, 2015, 36(1): 357-372. |
| LUO J S. Transition and prediction for hypersonic boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 357-372 (in Chinese). | |
| 12 | FEDOROV A V, KHOKHLOV A P. Receptivity of hypersonic boundary layer to wall disturbances[J]. Theoretical and Computational Fluid Dynamics, 2002, 15(4): 231-254. |
| 13 | 李学良, 李创创, 苏伟, 等. 分布式粗糙元对高超声速边界层不稳定性的影响试验[J]. 航空学报, 2024, 45(2): 128627. |
| LI X L, LI C C, SU W, et al. Experiment of influence of distributed roughness elements on hypersonic boundary layer instability[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128627 (in Chinese). | |
| 14 | 杨鹏, 唐志共, 陈坚强, 等. 高超声速有攻角锥飞行工况下迎风面波包的演化[J]. 航空学报, 2021, 42(S1): 726367. |
| YANG P, TANG Z G, CHENG J Q, et al. Temporal evolution of wavepackets on the windward side of an inclined hypersonic cone under a flight condition[J]. Acta Aeronautica et Astronautica Sinica. 2021, 42(S1): 726367 (in Chinese). | |
| 15 | MA Y B, ZHONG X L. Receptivity of supersonic boundary layer over a flat plate[C]∥41st Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2003: 788. |
| 16 | FEDOROV A V. Receptivity of a high-speed boundary layer to acoustic disturbances[J]. Journal of Fluid Mechanics, 2003, 491: 101-129. |
| 17 | MASLOV A A, SHIPLYUK A N, SIDORENKO A A, et al. Leading-edge receptivity of a hypersonic boundary layer on a flat plate[J]. Journal of Fluid Mechanics, 2001, 426(1): 73-94. |
| 18 | KARA K, BALAKUMAR P, KANDIL O. Effects of wall cooling on hypersonic boundary layer receptivity over a cone[C]∥ 38th Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2008: 3734. |
| 19 | BALAKUMAR P. Receptivity of hypersonic boundary layers to acoustic and vortical disturbances (invited)[C]∥45th AIAA Fluid Dynamics Conference. Reston: AIAA, 2015: 2473. |
| 20 | DUAN L, CHOUDHARI M M, CHOU A, et al. Characterization of freestream disturbances in conventional hypersonic wind tunnels[J]. Journal of Spacecraft and Rockets, 2019, 56(2): 357-368. |
| 21 | BALAKUMAR P, CHOU A. Transition prediction in hypersonic boundary layers using receptivity and freestream spectra[J]. AIAA Journal American Institute of Aeronautics and Astronautics, 2018, 56(1): 193-208. |
| 22 | ZHONG X L. Effect of nose bluntness on hypersonic boundary layer receptivity over a blunt cone[C]∥ 35th AIAA Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2005: 5022. |
| 23 | WHEATON B, JULIANO T, BERRIDGE D, et al. Instability and transition measurements in the Mach-6 quiet tunnel[C]∥39th AIAA Fluid Dynamics Conference. Reston: AIAA, 2009: 3559. |
| 24 | CHOU A. Characterization of laser-generated perturbations and instability measurements on a flared cone[D]. West Lafayette: Purdue University, 2010: 3-4. |
| 25 | CHOU A, WHEATON B, WARD C, et al. Instability and transition research in a Mach-6 quiet tunnel[C]∥ 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2011: 283. |
| 26 | HUANG Y, ZHONG X. Numerical study of hypersonic boundary-layer receptivity and stability with freestream hotspot perturbations[J]. American Institute of Aeronautics & Astronautics, 2016, 52(12):2652-2672. |
| 27 | HEITMANN D, RADESPIEL R. Simulation of the interaction of a laser generated shock wave with a hypersonic conical boundary layer[C]∥41st AIAA Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2011: 3875. |
| 28 | 江贤洋, 李存标. 高超声速边界层感受性研究综述[J]. 实验流体力学, 2017, 31(2): 1-11. |
| JIANG X Y, LI C B. Review of research on the receptivity of hypersonic boundary layer[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 1-11 (in Chinese). | |
| 29 | KARA K, BALAKUMAR P, KANDIL O. Receptivity of hypersonic boundary layers due to acoustic disturbances over blunt cone[C]∥45th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2007: 945. |
| 30 | 孙晓峰, 董旭, 张光宇, 等. 特征值理论在稳定性预测中的应用研究进展[J]. 航空学报, 2022, 43(10):527408. |
| SUN X F, DONG X, ZHANG G Y, et al. Progress review of application of eigenvalue theory to stability prediction[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 527408 (in Chinese). | |
| 31 | 万兵兵. 考虑熵层高超声速钝头体边界层的感受性问题研究[D]. 天津: 天津大学, 2018. |
| WAN B B. Study on sensitivity of hypersonic blunt body boundary layer considering entropy layer[D]. Tianjin: Tianjin University, 2018 (in Chinese). | |
| 32 | HUANG Y, ZHONG X. Numerical study of freestream hot-spot perturbation on boundary-layer receptivity for blunt compression-cones in Mach-6 flow[C]∥41st AIAA Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2011: 3078. |
| 33 | FEDOROV A, SHIPLYUK A, MASLOV A, et al. Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating[J]. Journal of Fluid Mechanics, 2015, 769: 99-728. |
| 34 | 刘智勇, 禹旻, 杨武兵. 温度对高速平板边界层转捩雷诺数的影响[J]. 空气动力学学报, 2020, 38(2): 308-315. |
| LIU Z Y, YU M, YANG W B. Effect of temperature on the transitional Reynolds number of high-speed planar boundary layer[J]. Acta Aerodynamica Sinica. 2020, 38(2): 308-315 (in Chinese). | |
| 35 | 梁贤. 高超声速钝锥边界层稳定性特征[D]. 上海: 上海大学, 2010. |
| LIANG X. Stability characteristics of hypersonic blunt cone boundary layer[D]. Shanghai: Shanghai University, 2010 (in Chinese). | |
| 36 | SCHNEIDER S P. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels[J]. Progress in Aerospace Sciences, 2015, 72: 17-29. |
| 37 | MARINEAU E C. Prediction methodology for second-mode-dominated boundary-layer transition in wind tunnels[J]. AIAA Journal, 2016, 55(2): 484-499. |
| [1] | Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN. Direct numerical simulation of hypersonic cone-flare model at angle of attack [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610. |
| [2] | Yalu FU, Xianxu YUAN, Pengxin LIU, Ming YU. Statistical properties of thermodynamic fluctuations in compressible wall⁃bounded turbulence [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 127217-127217. |
| [3] | Yang ZHANG, Jiaqi LUO, Xian ZENG. Elliptic flow noise by improved ghost⁃cell immersed boundary method [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128418-128418. |
| [4] | Junyang LI, Pengxin LIU, Ming YU, Dong SUN, Siwei DONG, Xianxu YUAN. Effects of viscous dissipation on wall heat flux in high-enthalpy turbulent boundary layer [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528963-528963. |
| [5] | Xiaodong LIU, Pengxin LIU, Chen LI, Dong SUN, Xianxu YUAN. Direct numerical simulation of high enthalpy shock wave/turbulent boundary layer interaction [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 127832-127832. |
| [6] | Yiming WU, Siyi QIU, Yang XIANG, Hong LIU. Mode evolution characteristics of isolated wing tip vortex: Experimental study [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(11): 127658-127658. |
| [7] | LI Qiang, WAN Bingbing, YANG Kai, ZHU Tao. Experimental research on characteristics of pressure and heat flux fluctuation in hypersonic cone boundary layer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 124956-124956. |
| [8] | SHEN Pengfei, LIU Pengxin, SUN Dong, YUAN Xianxu. Statistical characteristics of skin friction of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach 6 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 626005-626005. |
| [9] | DUAN Junyi, TONG Fulin, LI Xinliang, LIU Hongwei. Decomposition of mean friction drag in compression-expansion turbulent boundary layer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 625915-625915. |
| [10] | LIU Pengxin, YUAN Xianxu, LIANG Fei, LI Chen, SUN Dong. Quadrant decomposition analysis of fluctuations in high-temperature turbulent boundary layer with chemical non-equilibrium [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726338-726338. |
| [11] | LI Qing, TU Guohua, YU Zhaosheng, LIN Zhaowu, LI Tingting, YUAN Xianxu. Inertial particle transport in non-uniform accelerated flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726390-726390. |
| [12] | SUN Dong, LIU Pengxin, SHEN Pengfei, TONG Fulin, GUO Qilong. Direct numerical simulation of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach number 6 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124681-124681. |
| [13] | CHENG Zepeng, QIU Siyi, XIANG Yang, SHAO Chun, ZHANG Miao, LIU Hong. Evolution mechanism of instability features of wingtip vortex pairs based on bi-global linear stability analysis [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 123751-123751. |
| [14] | TONG Fulin, ZHOU Guiyu, SUN Dong, LI Xinliang. Expansion effect on shock wave and turbulent boundary layer interactions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 123731-123731. |
| [15] | TONG Fulin, SUN Dong, YUAN Xianxu, LI Xinliang. Direct numerical simulation of impinging shock wave/turbulent boundary layer interactions in a supersonic expansion corner [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 123328-123328. |
| Viewed | ||||||
|
Full text |
|
|||||
|
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341

