Design and Analysis of CFD Experiments for the Development of Bulk-Flow Model for Staggered Labyrinth Seal

<div>Static pressure distribution in the seal cavities and discharge coefficients in the seal orifices for the test number 1 (seal diameter = 220 mm, pressure drop = 50 bar, inlet preswirl = 1.9, and rotor peripheral velocity = 66.19 m/s).</div>

International Journal of Rotating Machinery

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Figure 18

Figure 18: Design and Analysis of CFD Experiments for the Development of Bulk-Flow Model for Staggered Labyrinth Seal 