Experimental Investigation and Numerical Simulation of Secondary Combustor Flow in Boron-Based Propellant Ducted Rocket

Author:

HU Jianxin,XIA Zhixun,WANG Dequan,HUANG Liya

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference15 articles.

1. 1) King, M. K.: Ignition and Combustion of Boron Particles and Clouds, J. Spacecraft Rockets, 19 (1982), pp. 294-306.

2. 2) Zhang, W., Fang, D. Y. and Xia, Z. X.: Numerical Study of Turbulent Flow in Unchoked Solid Ducted Rocket Combustor, AIAA Paper 2000-3729, 2000.

3. 3) Hu, J. X., Xia, Z. X., Wang, Z. J., Guo, J. and Zhang, W.: Experimental Investigation and Numerical Simulation of Secondary Chamber Flow in SDR, AIAA Paper 2004-3306, 2004.

4. 4) Chuang, C. L., Cherng, D. L. and Hsienh, W. H.: Study of Flowfield Structure in a Simulated Solid-Propellant Ducted Rocket, AIAA Paper 89-2507, 1989.

5. 5) Lazar, T. C., Venkateswaran, S. and Paul, P. J.: Flow Measurements in a Model Ramjet Secondary Combustion Chamber, J. Propul. Power, 6 (1990), pp. 727-731.

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