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  • 29-05-2024
  • Engineering
Answered

Calculate the thrust of the turbojet engine in Example 7.1 at M0 1/4 0.8, 9-m altitude, reduced throttle ( Tt4 1/4 1100K ) , and P0/P9 1/4 1 for a reference air mass flow rate of 50 / at a reference altitude of 12 m.

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