Design method of hedging flame jet pipe capable of forming uniform velocity field
A technology of uniform velocity and design method, applied in design optimization/simulation, chemical analysis using combustion, etc., can solve problems such as inability to guarantee the validity of experimental data, uneven outlet velocity distribution, impact of experimental data of rushing flame, etc., to achieve performance Ease of evaluation, quantification of actual performance, effect of avoiding flow separation
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Embodiment 1
[0047] Embodiment 1 of the present invention discloses a design method for opposing flame nozzles that can form a uniform velocity field, such as figure 1 As shown, it includes a nozzle diverging section 1, a nozzle transition section 2, and a nozzle shrinking section 3.
[0048] In Embodiment 1 of the present invention, the geometrical parameters of nozzle constriction section 3 selected according to requirements include: the outlet diameter of nozzle constriction section 3 is 20 mm, the area contraction ratio of nozzle constriction section 3 is 6.25, and the nozzle constriction section 3 The length is 80mm.
[0049] According to the inlet diameter of the nozzle diverging section 1 and the outlet diameter of the nozzle constricting section 3 being 20 mm, the inlet diameter of the nozzle diffusing section 1 is determined to be 20 mm; the nozzle diffusing section 1 adopts a gradual expansion design, and according to the The area expansion ratio of the nozzle is the same as the...
Embodiment 2
[0076] Embodiment 2 of the present invention discloses a design method for opposing flame nozzles that can form a uniform velocity field, such as figure 1 As shown, it includes a nozzle diverging section 1, a nozzle transition section 2, and a nozzle shrinking section 3.
[0077] In Embodiment 2 of the present invention, the geometrical parameters of nozzle constriction section 3 selected according to requirements include: the outlet diameter of nozzle constriction section 3 is 30mm, the area shrinkage ratio of nozzle constriction section 3 is 4, and the nozzle constriction section 3 The length is 100mm.
[0078] According to the inlet diameter of the nozzle diverging section 1 and the outlet diameter of the nozzle constricting section 3 being 30 mm, the inlet diameter of the nozzle diffusing section 1 is determined to be 30 mm; the nozzle diffusing section 1 adopts a gradual expansion design, and according to the The area expansion ratio of the nozzle is the same as the area...
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