Low-Frequency Feed-System-Coupled Combustion Instability in Hybrid Rocket Motors

The low-frequency unstable combustion of hybrid rocket motors was investigated using the transfer function of the full thermal-combustion-gasdynamic coupled system that was coupled with a liquid oxidizer feed system. This transfer function was obtained based on the method developed by Karabeyoglu et...

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Bibliographic Details
Main Authors: Takakazu MORITA, Saburo YUASA, Koki KITAGAWA, Toru SHIMADA, Shigeru YAMAGUCHI
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2013-07-01
Series:Journal of Thermal Science and Technology
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/jtst/8/2/8_380/_pdf/-char/en