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Flamelet Analysis for Transient Response to Pressure Oscillations  

Bae, Jun-Kyung (한양대학교 기계공학과)
Kim, Yong-Mo (한양대학교 기계공학과)
Kim, Seong-Ku (한국항공우주연구원)
Publication Information
Journal of the Korean Society of Combustion / v.16, no.1, 2011 , pp. 30-35 More about this Journal
Abstract
This study has been mainly motivated to numerically investigate the transient flame response to pressure oscillations in the gaseous hydrogen - liquid oxygen flames at supercritical pressures. The present analysis is based on the real-fluid transient flamlet model and the flame field is acoustically perturbed only by the sinewave oscillations in the frequency range from 1,000 Hz to 5,000 Hz. Based on numerical results, the detailed discussions are made for the flame response characteristics and the transient flamelet response associated with the high-frequency combustion instability in the liquid propellant rocket engines.
Keywords
Combustion instability; Gaseous hydrogen-liquid oxygen flame; Acoustic response; Super critical pressure; Flamelet approach; Real fluid effects;
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