Fine Measurement Experiment of Internal Flow Field in Ablated C-SiC Isolator
1.Beijing Bureau of Naval General Armaments Department,Beijing 100074,China;2.State Key Laboratory of Laser Propulsion and Application,Beijing Power Machinery Institute,Beijing 100074,China
CONG Kai1, CAO Xue-bin2, MAN Yan-jin2, ZHU Shou-mei2. Fine Measurement Experiment of Internal Flow Field in Ablated C-SiC Isolator[J]. Journal of Propulsion Technology, 2020, 41(10): 2180-2189.
[1] 曹学斌, 满延进, 李大进, 等. 畸变气流影响下C-SiC复合材料隔离段稳态特性试验研究[J]. 推进技术, 2018, 39(10): 2329-2339.
[2] 高亮杰, 张堃元, 曹学斌, 等 非对称来流下带粗糙度的隔离段实验研究[C]. 三亚:第四届全国高超声速科技学术会议, 2011.
[3] Waltrup P J, Billig F S. Structure of Shock Waves in Cylindrical Ducts[J]. AIAA Journal, 1973, 11(10): 1404-1408.
[4] Sullins G, Mc Lafferty G H. Experimental Results of Shock Train in Rectangular Ducts[R]. AIAA 92-5103.
[5] Hui-jun Tan, Shu Sun. Preliminary Study of Shock Train in a Curved Variable-Section Diffuser[J]. Journal of Propulsion and Power, 2008, 24(2): 245-252.
[6] 王成鹏, 张堃元, 金志光. 非均匀超声来流矩形隔离段内流场实验[J]. 推进技术, 2004, 25(4): 349-353.
[7] 卢洪波. 高超声速进气道典型热负荷区的流动特性研究[D]. 北京: 中国科学院力学研究所, 2014.
[8] 曹学斌, 满延进, 李大进, 等. 烧蚀后C-SiC复合材料隔离段内激波串长度预测[J]. 推进技术, 2019, 40(2): 285-294.
[9] Ikuit T, Mtsuo K, Nagai M, et al. Oscillation Phenomena of Pseudo-Shock Waves[J]. Bulletin of the Japan Society of Mechanical Engineers, 1974, 17(112): 1278-1285.
[10] Yamane R, Kondo E, Tomita Y, et al. Vibration of Pseudo-Shock in Straight Duct[J]. Bulletin of the Japan Society of Mechanical Engineers, 1984, 7(229): 1385-1398.
[11] Sugiyama H, Takeda H, Zhang J, et al. Locations and Oscillation Phenomena of Pseudo-Shock Waves in a Straight Rectangular Duct[J]. The Japan Society of Mechanical Engineers International Journal, Series 2, 1988, 31 (1): 9-15.
[12] 曹学斌, 张堃元, 王成鹏. 非对称来流下隔离段动态压力特性[J]. 推进技术, 2009, 30(1): 57-62.
[13] 曹学斌, 张堃元. 超燃冲压发动机隔离段非对称来流下激波串受迫振荡流动研究[J]. 空气动力学学报, 2011, 29(2): 135-141.
[14] Carroll B F, Dutton J C. Characteristics of Multiple Shock Wave/Turbulent Boundary Layer Interactions in Rectangular Ducts[J]. Journal of Propulsion and Power, 1990, 6(2): 186-193.
[15] Wagner J L, Yuceil K B, Valdivia A, et al. PIV Measurements of the Unstart Process in a Supersonic Inlet/Isolator[R]. AIAA 2008-3849.
[16] Wagner J L, Yuceil K B, Clemens N T. PIV Measurements of Unstart of an Inlet-Isolator Model in a Mach 5 Flow[R]. AIAA 2009-4209.
[17] 马 静. 超燃冲压发动机内流通道冷态流场的PIV试验研究[D]. 南京: 南京航空航天大学, 2011.
[18] 曹学斌, 朱守梅, 满延进, 等. 考虑进气道喉道非均匀流场影响的隔离段直连试验[J]. 推进技术, 2015, 36(4): 547-555.
[19] ZHAO YuXin, YI ShiHe, TIAN LiFeng, et al. Supersonic Flow Imaging Via Nanoparticles[J]. Science in China: E, 2009, 52(12): 3640-3648.
[20] 赵玉新, 易仕和, 田立丰, 等. 基于纳米粒子的超声速流动成像[J]. 中国科学 E 辑: 技术科学, 2009, 39 (12): 1911-1918.
[21] 易仕和, 何 霖, 田立丰, 等. 纳米示踪平面激光散射技术在激波复杂流场测量中的应用[J]. 力学进展, 2012, 42(2): 197-205.
[22] Zhi Chen, Yi Shihe, Zhu Yangzhu, et al. Investigation on Flows in a Supersonic Isolator with an Adjustable Cowl Convergence Angle[J]. Experimental Thermal and Fluid Science, 2014, 52: 182-190.
[23] 朱 华, 姬翠翠. 分形理论及其应用[M]. 北京: 科学出版社, 2011.
[24] 赵玉新, 易仕和, 田立丰, 等. 超声速湍流混合层实验图像的分形度量[J]. 中国科学 G 辑, 2008, 38(5): 562-571.
[25] 黄真理. 湍流的分形特征[J]. 力学进展, 2000, 30(4): 581-592.
[26] Sreenivasan K R. Fractals and Multifractals in Fluid Turbulence[J]. Annual Review of Fluid Mechanics, 1991, 23: 539-600.