Mixing spray pipe runner wall face determination method, mixing spray pipe and supersonic speed mixing wind tunnel
A definite method and technology of mixed injection, which is applied in the direction of measuring devices, instruments, aerodynamic tests, etc., can solve the difficulty of analyzing experimental data, the quality of the flow field at the exit section of the mixing nozzle, and the inability to design the three-dimensional mixing channel for mixing efficiency and other issues to achieve the effect of improving the mixing efficiency
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[0044] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in many different ways defined and covered by the claims.
[0045] figure 1 is a schematic diagram of a supersonic mixing wind tunnel according to the present invention. Such asfigure 1 As shown, the supersonic mixing wind tunnel of the present invention includes a transition section 10 , a stabilization section 20 , a nozzle section 30 , an experiment section 40 , and a diffuser section 50 connected in sequence.
[0046] figure 2 and image 3 A schematic structure of a transition section of a supersonic mixing wind tunnel according to the present invention is shown. Such as figure 2 and image 3 As shown, the inlet 11 of the transition section 10 is circular and transitions to a square outlet 12 for preliminary rectification of the gas.
[0047] Figure 4 and Figure 5 A schematic structure of a s...
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