November 02 (Thursday)
WISET 팀제 결과발표회 심화과정(II)
Oral,
제1발표장(201A호),
09:50~10:50
  • Chair :
Th01B-1
09:50~10:50
스월 강도에 따른 하이브리드 로켓의 연소 불안정 영향
이설하, 김지은, 김지혜, 유민정, 한송이, 이창진(건국대학교)
In this study, the effect of swirl injection on the combustion stability was investigated with experimental tests and numerical calculation. As a result, swirl injection seems to modify two main physical processes responsible for the occurrence of the LFI. With swirl injection, even the frequency characteristics of p′ and q′ of both 20Hz and 500Hz band were not changed. However, as the swirl intensity increases, the phase difference p′ and q′ in 500 Hz band showed an increase above π/2 showing a totally independent relation between p′ and q′. Therefore, it is believed that phase shift happened as the result of the complicate interaction of strong rotational flow structure near core region and the additional combustion in post chamber.
Keywords : Hybrid Rocket(하이브리드 로켓), Low Frequency Instability(저주파수 연소 불안전성), Swirl(스월)
Paper : Th01B-1.pdf

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