What is the resulting strain of the wire when it is used

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Company wants to use a 100 m long steel cable to pull an airplane glider. If the glider has a mass of 1000 kg, and assuming the load is given by F=mg = 9800 N, and if the Young’s modulus of steel is 200 GPa (200,000,000,000 Pa), and Poisson’s ratio is 0.3:

a) If you want the stress on the wire to equal half the yield stress (yield stress is 200 MPa= 200,000,000 Pa), what is the diameter of the wire you would choose (assume the wire has a circular cross-section)?

b) What is the resulting strain of the wire when it is used?

c) What is the change in length?

d) How much does the diameter change?

e) In a few words, explain the deformation mechanism that primarily occurs at small elastic tensile strains.

f) What is the largest allowable size surface crack/notch/scratch on the cable? Assume the highest stress occurs during takeoff when the force is due to the weight of the plane (9800 N), assume Y=1, and K1c of this alloy is 60 Mpa – m0.5

Reference no: EM13711478

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