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SHAFT IN PARALLEL:
SHAFT IN PARALLEL: The shaft are in parallel when the driving torque is applied at
the junction of shafts and resisting torque is at other ends of the shafts. Here, angle of twist is same for each shaft, but applied torque is divided between the 2 shaft.
i.e. θ1 = θ 2 and T = T1 + T2
if shaft are made of same material than G1 = G2
Such situation (θ1 = θ2 and T = T1 + T2) also arises when shaft ends are fixed and are subjected to a torque at common junction. As shown in figure given below
The wing of a light, single-engine general aviation aircraft has an area of 15.8 m 2 and a span of 9.6 m. The airfoil of the wing is NACA 65-415, which has a lift slope of 0.1033
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as diesel engine gives more milege than petrol engine then why we are using petrol engine..
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have assignment in FEM calculation and ANSYS are you able to solve this kind of assignment
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