se calculations also assume
    that the bypass flow is greater than the bleed flow.
</p>
<p>
    The area ratio between the exit area and critical area is determined by
    using the following equation:

    $$\textit{Ae_o_Acr} = \frac{\textit{Tcr_o_Te}^\frac{\gamma+1}{2(\gamma-1)}}{Me}$$

    in which the temperature ratio is determined by:

    $$\textit{Tcr_o_Te} = \frac{2}{\gamma+1}*[1+0.5*(\gamma-1)*Me^2]$$

    and the exit Mach number is determined by:

    $$ Me = \sqrt{\frac{2}{\gamma-1}*\left[\le