Design method for three-dimensional internal rotary inlet based on complete flow direction suction
A design method and air inlet technology, applied to the air inlet of turbine/propulsion device, calculation, combustion air/combustion-air treatment, etc., can solve the problem of reducing outlet uniformity, boundary layer separation, complex wave system structure etc. to achieve the effect of improving the self-starting performance
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[0023] Such as Figure 1-7 As shown, the marks in the figure are: 1 indicates the reference surface of the three-dimensional inward turning inlet, 2 indicates the position of the leading edge point of the three-dimensional inward turning inlet, 3 indicates the effective part of the basic flow field streamline, and 4 indicates the reflected shock wave , 5 represents the lip of the three-dimensional inward turning inlet, 6 represents the incident shock wave at the entrance of the three-dimensional inward turning inlet, 7 represents the centerline of the basic flow field rotation, 8 represents the intersection of the streamline and the reflected shock wave, and 9 represents the three-dimensional inward turning The shape line of the inlet shoulder, 10 represents the capture shape of the leading edge of the three-dimensional inward turning inlet, 11 represents the streamline tracked by the streamline tracking method, 12 represents the discrete point set of the effective part of the ...
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