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손채훈,Sohn, Chae-Hoon 대한기계학회 2002 大韓機械學會論文集B Vol.26 No.7
Acoustic behavior in baffled combustion chambers is numerically investigated by adopting linear acoustic analysis. Partial blade baffle, which is a variant of blade baffle, and hub-blade baffle with six blades are employed as baffle models. Through modal analysis, natural frequencies of each acoustic mode in baffled chambers are calculated and the reduction in natural frequencies caused by baffle installation is examined. Through harmonic analysis, acoustic pressure responses of each chamber to acoustic oscillating excitation are shown. The first tangential mode is found to be most sensitive to acoustic oscillation. Acoustic damping effect of baffle is quantified by damping factor. Damping effect of hub-blade baffle is the most appreciable and damping factor of partial blade baffle is much lower than that of blade baffle. Damping effect of six-blade baflle on the second tangential mode is as much as on the first tangential mode and hub-blade baffle can damp out appreciably the first tangential as well as the first radial mode with the aid of hub.
복사 열손실로 인한 확산 화염의 맥동 불안정에 관한 연구
손채훈,김종수,Sohn, Chae Hoon,Kim, Jong Soo 대한기계학회 1999 大韓機械學會論文集B Vol.23 No.9
Radiation-induced oscillatory instability in diffusion flames is numerically investigated with nonlinear dynamics considered. As the simplest flame model, a diffusion flame established in the stagnant mixing layer is employed with optically thin gas-phase radiation and unity Lewis numbers for all species. Attention is focused on the radiation-induced extinction regime, which occurs at large $Damk\ddot{o}hler$ number. Once the steady flame structure is obtained for a prescribed value of the initial $Damk\ddot{o}hler$ number, transient solution of the flame is calculated after a finite amount of the $Damk\ddot{o}hler$-number perturbation is imposed on the steady flame. Transient evolution of the flame exhibits three types of flame-evolution behaviors, namely decaying oscillatory solution, diverging solution to extinction and stable limit-cycle solution. A dynamic extinction boundary is identified for laminar flamelet library.
유체 공급 배관내 압력진동 감쇠에 미치는 오리피스의 음향학적 효과
손채훈(Chae-Hoon Sohn),김철희(Chul-Hee Kim) 한국항공우주학회 2006 韓國航空宇宙學會誌 Vol.34 No.4
유체 공급배관내의 압력진동을 감쇠할 수 있는 방법으로 배관내에 오리피스를 설치하는 방법을 채택하여, 그 압력진동 감쇠효과를 수치해석을 통해 조사하였다. 본 연구에서는, 압력진동의 진폭이 작다는 가정에 기초하여 오리피스의 음향학적 감쇠효과에 초점을 맞추었다. 오리피스의 위치에 따른 계산 결과로부터 압력진동의 마디, 즉 속도진동의 배가 되는 위치에 오리피스를 설치할 때 가장 효과적으로 압력 진동이 감쇠되었다. 이에 반해서, 오리피스를 압력진동의 배에 설치한 경우에는 오리피스의 설치 효과가 아주 미약하였다. 오리피스의 유로 봉쇄율이 증가함에 따라 감쇠효과는 단조적으로 증가하였고, 오리피스의 두께가 증가할수록 공진성을 약화시켜 감쇠효과가 크게 나타났다. 또한, 직경이 작은 배관에서 감쇠 효과가 더 크게 나타났다. Effects of an orifice on suppression of pressure oscillation in a fluid feeding line are investigated numerically through the installation of an orifice inside the feeding line. Based on linear acoustic theory, acoustic-damping effect of an orifice is emphasized in this study. When an orifice is installed at the node of pressure oscillation corresponding to the anti-node of velocity oscillation, damping capacity is maximized. On the other hand, the orifice installed at the anti-node of pressure oscillation has little damping capacity. As the blockage ratio and thickness of an orifice increase in the feeding line, damping factor increases. The feeding line with smaller diameter has more damping capacity, but damping factor increases more appreciably with blockage ratio in the feeding line with larger diameter.