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calculate the mass flow of the turbofan at an altitude of 1 0 , 6 0 0 m Ca 8 0 mach , E 7

calculate the mass flow of the turbofan at an altitude of 10,600 m Ca 80 mach
, E 74kn, Rp 24, Rfan 1.28, B 4, Ni 93%Nc (9%, Nt ((%, Nm 97%, Nj)8%, Pcc 3%, Tmax1380K

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