Question: When the thrust available variation is given by T A ( T A ) V = 0 = A M - n , develop an

When the thrust available variation is given by TA(TA)V=0=AM-n, develop an
analytical solution for the calculation of maximum rate of climb. Compare this with
the simpler analytical approach discussed in Section 5.10.2 for the case of constant
thrust available.
When the thrust available variation is given by TA(TA)V=0=AM-n, develop an

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