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PASSlVE SHOCK CONTROL IN TRANSONIC FLOW FIELD  

Matsuo S (Dept. of Mechanical Engineering, Saga University)
Tanaka M (Dept. of Mechanical Engineering, Saga University)
Setoguchi T (Dept. of Mechanical Engineering, Saga University)
Kashimura H (Dept. of Control and Information System Engineering, Kitakyushu National College of Technology)
Yasunobu T (Dept. of Control and Information System Engineering, Kitakyushu National College of Technology)
Kim H.D (School of Mechanical Engineering College of Natural Science, Andong National University)
Publication Information
Journal of computational fluids engineering / v.10, no.1, 2005 , pp. 80-86 More about this Journal
Abstract
In order to control the transonic flow field with a shock wave, a condensing flow was produced by an expansion of moist air on a circular bump model and shock waves were occurred in the supersonic parts of the fields. Furthermore, the additional passive technique of shock-boundary layer interaction using the porous wall with a cavity underneath was adopted in this flow field. The effects of these methods on the shock wave characteristics were investigated numerically. The result showed that the flow fields might be effectively controlled by the suitable combination between non-equilibrium condensation and the position of porous wall.
Keywords
Compressible Flow; Non-Equilibrium Condensation; Boundary Layer; Flow Control;
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