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Compute and plot with extraordinary neatness and professionalism (i.e. generate plots using a computer) the specific thrust and specific fuel consumption versus the design compressor

Compute and plot with extraordinary neatness and professionalism (i.e. generate plots using a computer) the specific thrust and specific fuel consumption versus the design compressor pressure ratio for an ideal turbojet. Plot the results over the range of compressor pressure ratios from 1.0 to wherever the thrust becomes zero. Let the flight Mach number be 2.7

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