Study of Liquid Breakup Mechanism for Application of Solid Rocket Propulsion
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-10-7473-8_16
Reference7 articles.
1. Y.-H. Yena, R. Amano, Investigation of alumina flow breakup process in solid rocket propulsion chamber. in 54th AIAA Aerospace Sciences Meeting, 2016, p. 0498
2. P. Thakre, V. Yang, Chemical erosion of refractory-metal nozzle inserts in solid-propellant rocket motors. J. Propul. Power 25, 40–50 (2009)
3. Y. Xiao, R. Amano, T. Cai, J. Li, New method to determine the velocities of particles on a solid propellant surface in a solid rocket motor. J. Heat Transf. 127, 1057–1061 (2005)
4. Y. Xiao, R. Amano, T. Cai, J. Li, G. He, Particle velocity on solid-propellant surface using X-ray real-time radiography. AIAA J. 41, 1763–1770 (2003)
5. A. Bandera, F. Maggi, L. DeLuca, Agglomeration of aluminized solid rocket propellants. AIAA Pap. 5439, 2009 (2009)
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