A Complete Parametric Cycle Analysis for Ideal TurboFan ...
Table 7.1 –Input data for Engine parameters (SI unit) Pressure drop ratio engine-core P0/P10 = 0.9 T0 = 216.6667 K engine - fan P0/P19 = 0.9 Total pressure ratio Maximum diffuser total pressure ratio d max = 0.99 Properties of air and fuel main burner total pressure ratio b = 0.96 Specific heat at constant pressure ITB - burner total pressure ... ................
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