Step 1: Calculate the velocity at the nozzle exit using the steady flow energy equation:
\[m_1 \cdot h_1 + \frac{v_1^2}{2000} = m_2 \cdot h_2 + \frac{v_2^2}{2000}\]
Given:
\(h_1 = 3025 \, \text{kJ/kg}\), \(v_1 = 60 \, \text{m/s}\), \(h_2 = 2790 \,
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