Based on Fluent Numerical Calculation of Refractive Index on Rocket Engine Nozzle Plume ()
Qiangfeng Huang,
Xiong Wan,
Zhimin Zhang,
Huaming Zhang,
Hengyang Shen,
Tingting Du
1Key Laboratory of Nondestructive Testing (Ministry of Education), Nanchang, Hangkong University, Nanchang, Jiangxi, China
2Key Laboratory of Spatial Active Opto-electronic Techniques, Shanghai Institute of Technical, Physics,
Chinese Academy of Sciences, Shanghai, China.
Key Laboratory of Nondestructive Testing (Ministry of Education), Nanchang, Hangkong University, Nanchang, Jiangxi, China.
DOI: 10.4236/opj.2013.32B023
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Abstract
Numerical 2D simulation and
research on internal flow field and external flow field of rocket motor nozzle
using FLUENT software. Analyze the flow condition of internal flow field and
external flow field, and according to add in the amount of the different gas components,
obtain the clear distribution of contour of density flow field, pressure flow
field and various material components and so on. Simulation results agree with
the results observed from the test on the ground, and provide reference for
solid rocket motor development.
Share and Cite:
Q. Huang, X. Wan, Z. Zhang, H. Zhang, H. Shen and T. Du, "Based on Fluent Numerical Calculation of Refractive Index on Rocket Engine Nozzle Plume,"
Optics and Photonics Journal, Vol. 3 No. 2B, 2013, pp. 90-93. doi:
10.4236/opj.2013.32B023.
Conflicts of Interest
The authors declare no conflicts of interest.
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