Define stagnation temperature. Air leaves the compressor of a jet engine at a temperature of
150°C, a pressure of 5 bar and a velocity of 120m/s. Determine the isentropic stagnation
temperature and pressure.
"T=T_0+\\frac{v^2}{c},"
"T=150+\\frac{120^2}{1005}=164\u00b0C."
"p=p_0\\cdot \\frac{T}{T_0},"
"p=5\\cdot \\frac{164}{150}=5.5~bar."
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