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58 Gas Turbine Handbook: Principles and Practices<br />

Figure 4-8. Rotating stall.<br />

ρ, and the change in velocity. From the velocity triangles the pressure<br />

rise per stage is determined.<br />

ÄP =<br />

ρ W 2<br />

2g 1 – W 2 2 + ρ C 2 2<br />

c 2g 2 – C 3<br />

c<br />

(4-19)<br />

This expression can be further simplified by combining the differential<br />

pressure and density, and referring to feet of head.<br />

Head = Ç g c<br />

ÄC = ÄP ρ (4-20)<br />

where ÄP ρ is the pressure rise across the stage and Head is the pressure<br />

rise of the stage measured in feet head of the flowing fluid. The<br />

standard equation for compressor head is given below.

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