Phase transition between pressure and heat release oscillations in hybrid rocket combustion

Author:

Choi Hyosang,Lee Changjin,Kang Sang Hun

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference20 articles.

1. R. M. Jenkins and J. R. Cook, A preliminary analysis of low frequency pressure oscillations in hybrid rocket motors, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, California, USA (1995) AIAA 95–2690.

2. A. Karabeyoglu, S. De Zilwa, B. Cantwell and G. Zilliac, Modeling of hybrid rocket low frequency instabilities, Journal of Propulsion and Power, 21 (6) (2005) 1107–1116.

3. K. S. Park and C. J. Lee, Low frequency instability in laboratory-scale hybrid rocket motors, Aerospace Science and Technology, 42 (2015) 148–157.

4. Y. J. Moon and C. J. Lee, Dynamics of post chamber flame and combustion pressure in hybrid rocket, 52nd AIAA Joint Propulsion Conference (AIAA 2016-4869) (2016).

5. D. Y. Kim and C. J. Lee, Destabilization of the shear layer in the post chamber of a hybrid rocket, Journal of Mechanical Science and Technology, 30 (4) (2016) 1671–1679.

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