Question: Please don't copy paste from another another persons work. It would help me out a lot if you could solve it step by step and

Please don't copy paste from another another persons work. It would help me out a lot if you could solve it step by step and explain in a couple of words what your process is. Thanks.

Please don't copy paste from another another
Discussion Problem Let us consider a cantilever wing clamped at one end (the fuselage) and free at the other. See the diagram below. Suppose the deflection of the wing is governed by the differential equation dy P =Q(2) ,0<: where i is the length of wing y deflection at a distance x from fuselage p proportional to constant compressive axial force acting on and q load x. also e young modulus elasticity material moment inertial cross section cross-sectional area uniform along suppose l="30" m. assuming gpa determine subject boundary conditions: hint: obtain general solution given differential equation first. then substitute conditions solve for constants solving an initial value problem>

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