Axial Compressors and Turbines

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Abstract

With the definition of the work coefficient in (6.4a) and (6.4b), we can now write from (4.22a) to (4.22d) the nondimensional azimuthal velocity component expressions as follows:$$ \frac{{{{c}_{\rm{u1}}}}}{u} = \left({1 - \hat{r}} \right) - \frac{\Psi}{4} $$ $$ \frac{{{{c}_{\rm{u2}}}}}{u} = \left({1 - \hat{r}} \right) + \frac{\Psi}{4} $$ $$ \frac{{{{w}_{\rm{u1}}}}}{u} = \hat{r} + \frac{\Psi}{4} $$

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Bose, T. (2012). Axial Compressors and Turbines. In Springer Aerospace Technology (pp. 163–195). Springer Nature. https://doi.org/10.1007/978-1-4614-3532-7_7

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