For the Gulfstream IV with the thrust available variations given by Eqs. (1) and (2) in Problem 5.18, analytically (directly) calculate Vmax at sea level and at 30,000 ft. Compare with the graphical results obtained in Problem 5.18. Comment on the increased level of difficulty of this calculation compared to that performed in Example 5.6 where the thrust was assumed constant with velocity.
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