Chart_18
Fig 30: Thermic efficiency, TSFC, and Thrust as function of BPR for a Turbofan with separated flux (βf=1.5, βc=20, Ta=290K, T4=1400K, M=0).
Fig 30: Thermic efficiency, TSFC, and Thrust as function of BPR for a Turbofan with separated flux (βf=1.5, βc=20, Ta=290K, T4=1400K, M=0).