Rotational flow distortion flow control device for S-shaped air inlet channel based on fluid oscillator
A technology of flow control and swirl distortion, applied in the direction of jet propulsion device, gas turbine device, turbine/propulsion device inlet, etc., can solve problems such as limited control range and inability to adjust excitation
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[0016] The invention proposes a flow control idea based on a figure-eight array fluid oscillator to control swirling flow distortion in an S-shaped inlet channel. see figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 As shown, the detailed implementation steps of this embodiment of the method design of the present invention are described below.
[0017] The fluid oscillators 3 are installed between the curved section 4 and the inlet stabilizing section 2, and are symmetrically distributed on the central plane of the inlet stabilizing section 2, and the distribution positions and installation numbers of the fluid oscillators are individually adjustable.
[0018] The oscillating jet 11 flows out from the outlet 9 of the fluid oscillator and interacts with the airflow from the inlet stable section 2. Due to the velocity difference between the jet and the inlet stable section 2, the flow is sheared to the vortex, and then the vortex develops to the curved section 4 and i...
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