Question: An ideal gas flows adiabatically through a duct. At section 1, p1 = 140 kPa, T1 = 260°C, and V1 = 75 m/s. Farther downstream,
(a) Air, k = 1.4, and
(b) Argon, k = 1.67. Fig P9.1
pl 140 kPa TI = 260C V1 = 75 m/s p2 30 kPa T2 = 207
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a For air take k 140 R 287 Jkg K and cp 1005 Jkg K The adiabatic steadyflow energy equation 923 is ... View full answer
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