Jet Propulsion/General cascade analysis

From testwiki

Jump to navigation Jump to search

The total enthalpy h_t of the fluid flowing at velocity u is

$h_{t} = c_{p} T_{t} = c_{p} T + u^{2} / 2 = h + u^{2} / 2$

Euler turbine equation

stage temperature ratio

Retrieved from "https://en-labs.wikimedia.beta.math.wmflabs.org/w/index.php?title=Jet_Propulsion/General_cascade_analysis&oldid=731"

Jet Propulsion