I came with the following explanation, but I am not sure if it is correct. The variation of the thrust coefficient is directly related to the variation of the thrust force. According to the Newton’s second law, the aerodynamic forces are associated with the change in momentum of the fluid with time. This is equivalent to the mass times the velocity of the fluid. Then, the density depends on the mass airflow, that means a higher value of air density contains additional mass, which lead to a greater thrust force

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