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3.2 Isentropic Isothermal Flow Nozzle

$\displaystyle T_1 = T_2$ (26)





The star values

$\displaystyle T = T^{*}$ (31)

$\displaystyle { P \over P^{*}} = { \rho \over \rho^{*}} =$   e$\displaystyle ^{(1-M^2) k \over 2}$ (32)

$\displaystyle { A \over A^{*}} = {1 \over M}$   e$\displaystyle ^{(1-M^2) k \over 2}$ (33)



The initial stagnation temperature is denoted as $ {T_{0}}_{int}$.






for isothermal





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