Unsteady Transonic Flow Control around an Airfoil in a Channel
Hamid, M. A., Hasan, Abmt, Ali, M., Mitsutake, Y., Setoguchi, T. and Yu, S.1
2016
关键词transonic flow passive control shock wave oscillation moist air reduction bump Thermodynamics Engineering
中文摘要Transonic internal flow around an airfoil is associated with self-excited unsteady shock wave oscillation. This unsteady phenomenon generates buffet, high speed impulsive noise, non-synchronous vibration, high cycle fatigue failure and so on. Present study investigates the effectiveness of perforated cavity to control this unsteady flow field. The cavity has been incorporated on the airfoil surface. The degree of perforation of the cavity is kept constant as 30%. However, the number of openings (perforation) at the cavity upper wall has been varied. Results showed that this passive control reduces the strength of shock wave compared to that of baseline airfoil. As a result, the intensity of shock wave/boundary layer interaction and the root mean square (RMS) of pressure oscillation around the airfoil have been reduced with the control method.
内容类型期刊论文
源URL[http://ir.etp.ac.cn/handle/311046/113085]  
专题工程热物理研究所_Journal of Thermal Science_期刊论文
作者单位1.[Hamid, Md. Abdul
2.Hasan, A. B. M. Toufique
3.Ali, Mohammad] Bangladesh Univ Engn & Technol, Dept Mech Engn, Dhaka 1000, Bangladesh. [Mitsutake, Yuichi
4.Setoguchi, Toshiaki] Saga Univ, Inst Ocean Energy, Saga 8408502, Japan. [Yu, Shen] Chinese Acad Sci, Inst Engn Thermophys, POB 2706, Beijing 100080, Peoples R China.
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Hamid, M. A., Hasan, Abmt, Ali, M., Mitsutake, Y., Setoguchi, T. and Yu, S.. Unsteady Transonic Flow Control around an Airfoil in a Channel[J],2016.
APA Hamid, M. A., Hasan, Abmt, Ali, M., Mitsutake, Y., Setoguchi, T. and Yu, S..(2016).Unsteady Transonic Flow Control around an Airfoil in a Channel..
MLA Hamid, M. A., Hasan, Abmt, Ali, M., Mitsutake, Y., Setoguchi, T. and Yu, S.."Unsteady Transonic Flow Control around an Airfoil in a Channel".(2016).
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