Author_Institution :
State Key Lab. of Aerodynamics, China Aerodynamics R&D Center, Mianyang, China
Abstract :
Synthetic-Jet(SJ) technology is a novel method for flow control in aerodynamic design of aircrafts. With development of science and technology, flow control method based on SJ technology makes significant progress, and it is very useful. Furthermore, Synthetic-Jet actuator (SJA) has advantages of light weight, simple structure, no need for external air supply. With incessant requirements for high performances of spacecrafts, the application of active flow control technology, especially SJ technology, turns into one of the hottest research topics. In this paper, based on two-dimensional structured moving grids algorithm and multi-block grid technology, numerical simulation investigation about the effects of parameters on the performances of SJA is conducted. The research results indicate that the maximum jet velocity increases as the SJA vibration frequency and amplitude increase, and decreases as the orifice diameter increases. The orifice thickness has little influence on the maximum jet velocity. SJ flow presents turbulent characteristics at high Reynolds number (Re), and the increase of Re makes diameter of vortex core and attenuation speed greater, the increase of Strouhal number (St) makes diameter of vortex core smaller. In a word, the paper presents effects of different physical parameters, such as operating parameters, orifice parameters, Re, St, and so on, on flow characteristics of SJ. The results may provide technical support for the design and application of SJA.
Keywords :
aerodynamics; aircraft; flow control; flow simulation; jets; numerical analysis; space vehicles; turbulence; vibrations; vortices; SJ technology; SJA; SJA vibration amplitude decrement; SJA vibration frequency increment; Strouhal number; active flow control technology; aircraft aerodynamic design; maximum jet velocity; multiblock grid technology; numerical simulation; orifice diameter increment; orifice thickness; physical parameters; reynolds number; spacecrafts; synthetic-jet actuator; synthetic-jet technology; two-dimensional structured moving grid algorithm; vortex core diameter; Aerodynamics; Cavity resonators; Fluids; Numerical simulation; Orifices; Pistons; Vibrations; Active flow control; Numerical simulation; Parameters; Structured moving grids; Synthetic-Jet;