Help me pls with this exam question 

The air exiting the compression stage in an air standard turbojet engine is at 475K. If the air to fuel ratio is 35:1, find the maximum temperature (in K) for the engine. Assume LHV= 43.5 MJ/kg, cp=1005 J/kgK

Mathematical Physics
Jevil Jevil
1
Report
  • Daniel90 Daniel90
    +1

    It would take 15-20 minutes to answer this question, and it should come with a bounty.

Answer this question
Join Matchmaticians Affiliate Marketing Program to earn up to 50% commission on every question your affiliated users ask or answer.