Assignment activity and guidance Activity 1 A wing spar beam is subjected to vibrations along its length, emerging from two fuel pumps situated at opposite ends of the beam. The displacement

(in mm) caused by the vibrations can be modelled by the following equations, d₁ = 2.34 sin (100nt + 570 4 d₂= 3.46 sin (100mt 3 To understand the best type, size and location of fasteners to restrain the beam (for minimum ibration), you must analyse and calculate the effect of the vibrations along its length. onsidering the above displacement equations: i) State the amplitude, phase, frequency and periodic time of each of the above equations. ii) Determine how long it takes for each machine to first produce its maximum displacement (i.e. the first instance after t = 0 ms in either the positive or negative y-direction). ii) Use the compound angle formulae to expand d₁ and dz into the form a sin(100πt) ± ß cos (100nt), where a and ß are numbers to be found. -)Using your answers from the part (iii), express d₁+ d₂ in a similar form. Analytically, convert your answer from part (iv) into the equivalent form R sin(100nt + p).