No-moving-part hybrid-synthetic jet actuator

被引:130
作者
Tesar, V [1 ]
Hung, CH [1 ]
Zimmerman, WB [1 ]
机构
[1] Univ Sheffield, Dept Chem & Proc Engn, Proc Fluid Grp, Sheffield S1 3JD, S Yorkshire, England
基金
英国工程与自然科学研究理事会;
关键词
synthetic jets; hybrid-synthetic jets; fluidics; feedback loop; acoustic propagation;
D O I
10.1016/j.sna.2005.06.022
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In contrast to usual synthetic jets, the "hybrid-synthetic jets" of non-zero time-mean nozzle mass flow rate are increasingly often considered for control of flow separation and/or transition to turbulence as well as heat and mass transfer. The paper describes tests of a scaled-up laboratory model of a new actuator version, generating the hybrid-synthetic jets without any moving components. Self-excited flow oscillation is produced by aerodynamic instability in fixed-wall cavities. The return flow in the exit nozzles is generated by jet-pumping effect. Elimination of the delicate and easily damaged moving parts in the actuator simplifies its manufacture and assembly. Operating frequency is adjusted by the length of feedback loop path. Laboratory investigations concentrated oil the propagation processes taking place in the loop. (c) 2005 Published by Elsevier B.V.
引用
收藏
页码:159 / 169
页数:11
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