Inglês, perguntado por edisonosilva1841, 9 meses atrás

Air flows steadily and isentropically into an aircraft at a rate of 100 kg/s. At a section where the area is 0.464 m2 , Mach number, temperature and absolute pressure are found to be 3,-60oC and 15.0 kPa. Determine the velocity and cross-section area downstream where T

Soluções para a tarefa

Respondido por aaaa1234455
1
  1. Resposta:t54qaswderftgyhuo9p0-´pçolkijuytrewrftg4324244242342342343254324yhi

Explicação:

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