Effects of Repetitive Laser Energy Deposition on Supersonic Duct Flows

被引:15
作者
Hoang Son Pham [1 ]
Myokan, Manabu [1 ]
Tamba, Takahiro [1 ]
Iwakawa, Akira [1 ]
Sasoh, Akihiro [1 ]
机构
[1] Nagoya Univ, Dept Aerosp Engn, Chikusa Ku, Furo Cho, Nagoya, Aichi 4648601, Japan
关键词
UNSTEADY;
D O I
10.2514/1.J056190
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An experimental study was conducted to examine the effects of repetitive energy deposition on the supersonic flow characteristics over a duct system with a central conical compression surface. Boundary-layer separation on the compression surface could induce flow instability in pulsation and resonant modes. At subcritical operation, this flow instability became stronger and the "big buzz" phenomenon occurred. To control these undesirable operations, repetitive laser energy deposition was done with a repetition frequency of up to 60 kHz, which resulted in a reduction of flow separation on the compression surface. It was also observed that flow oscillation characteristics at the two modes were modified; total pressure inside the duct chamber was increased and the big buzz was significantly suppressed.
引用
收藏
页码:542 / 553
页数:12
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