Dear Researchers,

What are the criteria to identify the cruise condition for any turbojet engine?

How do I determine the cruise condition (altitude & Mach #) for the small-scale turbojet engine? based on the turbojet engine model is able to reach an altitude up to 1,000 m or 5,000 m, Mach# is 0.5 or 0.8.

Thanks in Advance,

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