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5-1) (15) Estimate the exit pressure of the convergent-divergent nozzle for stable supersonic flow in the high-pressure turbi

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isenAe Aa not aroa, A - erid anea h:1- Cavengenet-divent mozale 2(Y-1) (1+ 2 Aa Mc (1.441 2(1.4 1.4 2 1,4 41 71.4- 1 + 1.1 (1VeMenRTe 1 + ni) Te (- 2. O8OS Assuming Ti 33 K that T Gkd temperatu 33 K Te O80Sx T Te 670S6 1.4x287xO 805XT Ne 1x 13.78T Je

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