Critical pressure ratio for the flow of gases through a converging nozzle is given by (a) (left(frac{2}{gamma+1}
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Critical pressure ratio for the flow of gases through a converging nozzle is given by
(a) \(\left(\frac{2}{\gamma+1}\right)^{\gamma / \gamma-1}\)
(b) \(\left(\frac{1}{\gamma+1}\right)^{\gamma / \gamma-1}\)
(c) \(\left(\frac{2 \gamma}{\gamma+1}\right)^{\gamma / \gamma-1}\)
(d) None of these
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