Question: I Consider the following function f = Mx + Mx - 4xx + 4x where f is the aircraft fuel burn (objective function), M
I Consider the following function f = Mx + Mx - 4xx + 4x where f is the aircraft fuel burn (objective function), M is the Mach number, and x and x are the relative spans and chords of the wing (design variables), respectively. Conduct a multi-point optimization that can balance the fuel burn at Mach numbers 1 and 2. Note that the fuel burn at Mach numbers 1 and 2 are equally important. Requirements: a) Derive the multi-point optimization formulation, i.e., as a function of x and x (30%) b) Solve the multi-point optimization problem and report the optimal objective function f* and design variable x*. (70%)
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