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FLIGHT MECHANICS PROBLEM (a) Give a short explanation for CAS/Mach Climb regime and CAS/Mach transition altitude....

FLIGHT MECHANICS PROBLEM

(a) Give a short explanation for CAS/Mach Climb regime and CAS/Mach transition altitude.

(b) Derive the expression between drag D and speed V . Plot the V βˆ’ D graph for the given aircraft at 8000m and 10000m for level flight.

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