超音速钝体无粘绕流的计算

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (S1): 72-75.

• 论文 • Previous Articles Next Articles

CALCULATION OF SUPERSONIC INVISCID FLOW OVER BLUNT NOSED BODIES

Shen Xialing, Wu Zongcheng, Chen Yanqing

Institute of Fluid Mechanics,Beijing University of Aeronautics and Astronautics,Beijing,100083

Received:1996-01-25 Revised:1996-04-22 Online:1996-11-25 Published:1996-11-25

Abstract

Abstract: Numerical simulations of supersonic and hypersonic inviscid flow over blunt nosed bodies are investigated by an upwind scheme of the compatibility relations for the three dimensional method of characteristics. An inverse method is used to compute the flowfield behind the detached shock and the method of axisymmetric characteristics is used to determine flow parameters on the initial value surface.The results of numerical examples agree comparatively with the experimental data.

Key words: method of characteristics, supersonic flow, inviscid flow

CLC Number:

Shen Xialing;Wu Zongcheng;Chen Yanqing. CALCULATION OF SUPERSONIC INVISCID FLOW OVER BLUNT NOSED BODIES[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(S1): 72-75.

[1]	GANG Dundian, YI Shihe, MI Qi, NIU Haibo. Experiment on interaction between supersonic turbulent boundary layer and cylinder [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 626104-626104.
[2]	CHEN Jiazheng, HU Guotun, FAN Guochao, CHEN Weifang. Bow shock wave control and drag reduction by plasma synthetic jet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124773-124773.
[3]	CHEN Yile, YU Kaikai, XU Jinglei. New design method for scramjet nozzles with strong geometric constraints [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 124259-124259.
[4]	ZOU Dongyang, LIN Jingzhou, HUANG Jie, LIU Jun. Fitting algorithms for three dimensional flows with shock waves [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124141-124141.
[5]	YU Min, YANG Wubing, SHEN Qing. Mixing enhancement of supersonic wake shear layer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 625876-625876.
[6]	OUYANG Xiaosui, LIU Yi. Panel flutter of variable stiffness composite laminates in supersonic flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(3): 221539-221539.
[7]	QIAO Wenyou, YU Anyuan, YANG Dawei, LE Jialing. Integration design of inward-turning inlets based on forebody shock wave [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(10): 122078-122078.
[8]	XU Jinglei, SONG Youfu, ZHANG Yang, BAI Junqiang. Turbulence mixing length for compressible free shear flows [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(6): 1841-1850.
[9]	LIU Jun, ZOU Dongyang, DONG Haibo. A moving discontinuity fitting technique to simulate shock waves impinged on a straight wall [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 836-846.
[10]	YI Shihe, CHEN Zhi, ZHU Yangzhu, HE Lin, WU Yu. Progress on experimental techniques and studies of hypersonic/supersonic flows [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 98-119.
[11]	YANG Yue, YOU Jiaping, SUN Mingbo. Modeling of turbulence-chemistry interactions in numerical simulations of supersonic combustion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 261-273.
[12]	ZHUO Changfei, WU Xiaosong, FENG Feng. Effect of Base Bleed Type on Drag Reduction Performance in Supersonic Flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2144-2155.
[13]	GUO Shanguang, WANG Zhenguo, ZHAO Yuxin, FAN Xiaoqiang. Inverse Design of the Fore-body Curved Shock Wave of the Hypersonic Planar Inlet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1246-1256.
[14]	CHEN Qi, SI Fangfang, CHEN Jianqiang, YUAN Xianxu, XIE Yufei. Study of Protuberances in Supersonic Flow with RANS/LES Method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(7): 1531-1537.
[15]	YANG Zhanyu, SHAN Peng, ZHAO Lushun, JIE Ke, GUO Desan, LIU Jian, HUANG Yong. Experimental Study on Flame Holding Torch of a Hydrocarbon Fueled Combined Supersonic Combustor with a Pilot Burner and a Streamwise-vortices Generator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (3): 390-401.

CALCULATION OF SUPERSONIC INVISCID FLOW OVER BLUNT NOSED BODIES

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments