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斜出口合成射流激励器S进气道分离流动控制

李斌斌 程克明 顾蕴松

实验流体力学2012,Vol.26Issue(2):34-37,4.
实验流体力学2012,Vol.26Issue(2):34-37,4.

斜出口合成射流激励器S进气道分离流动控制

Separation flow control of beveled synthetic jet actuator in S-shaped inlet

李斌斌 1程克明 1顾蕴松1

作者信息

  • 1. 南京航空航天大学航空航天学院,江苏南京210016
  • 折叠

摘要

Abstract

Design and process a type of beveled synthetic jet actuator with single membrane and dual chambers, and its application in the S-shaped inlet active flow control has been studied by using PSI DTC initium pressure scanning system. The results show that beveled synthetic jet actuator can suppress flow separation in S-shaped inlet, improve the total pressure recovery coefficient σ and reduce the pressure distortion DC90. Only by changing the actuator operating voltage and frequency, the flow control can be achieved within the S inlet. At the resonance frequency of synthetic jet actuator and the stream velocity V=80m/s, using beveled synthetic jet actuator can increase the total pressure recovery coefficient by 0. 37%, when the energy consumption of synthetic jet is only 0. 24% of the main stream.Design and process a type of beveled synthetic jet actuator with single membrane and dual chambers, and its application in the S-shaped inlet active flow control has been studied by using PSI DTC initium pressure scanning system. The results show that beveled synthetic jet actuator can suppress flow separation in S-shaped inlet, improve the total pressure recovery coefficient σ and reduce the pressure distortion DC90. Only by changing the actuator operating voltage and frequency, the flow control can be achieved within the S inlet. At the resonance frequency of synthetic jet actuator and the stream velocity V=80m/s, using beveled synthetic jet actuator can increase the total pressure recovery coefficient by 0. 37%, when the energy consumption of synthetic jet is only 0. 24% of the main stream.

关键词

斜出口合成射流激励器/S进气道/边界层分离/流场测量/流动控制

Key words

beveled synthetic jet actuator/S-shaped inlet/boundary layer separation/flow field measurement/ flow control

分类

数理科学

引用本文复制引用

李斌斌,程克明,顾蕴松..斜出口合成射流激励器S进气道分离流动控制[J].实验流体力学,2012,26(2):34-37,4.

实验流体力学

OA北大核心CSCDCSTPCD

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