Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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Here are the dimensions, sorry for not having them earlier b = 0.4 m, d =0.5 m , t =0.1 m.
3) The force, FT = 1 kN, and moment, MT = 0.5 kN-m, at the tip are caused by a wing tip vortex
and a winglet, not shown. L = 12 m and the spar has an elastic modulus of E = 70 GPa and a
Poisson’s ratio of
n = 0.33. The mass of the wing is 4000 kg, and the weight of the engine is 107
kN. Use 9.8 m/s 2 for the acceleration due to gravity.
a) The aerodynamic center for problem 3 is 0.1 m from the y axis (neutral axis). Calculate the
twist angle caused by the lift force.
b) For problem 3, calculate the reactions at the fixed end.
and a winglet, not shown. L = 12 m and the spar has an elastic modulus of E = 70 GPa and a
Poisson’s ratio of
n = 0.33. The mass of the wing is 4000 kg, and the weight of the engine is 107
kN. Use 9.8 m/s 2 for the acceleration due to gravity.
a) The aerodynamic center for problem 3 is 0.1 m from the y axis (neutral axis). Calculate the
twist angle caused by the lift force.
b) For problem 3, calculate the reactions at the fixed end.
c) Assume the engine in problem 3, applies a torque around the x – axis of the spar of 100 kN-m,
calculate the angular delfection of the wing at x = 3 m due to the engine.
calculate the angular delfection of the wing at x = 3 m due to the engine.
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Step 1: Determine the twist angle, the reactions at the fixed end, and angular deflection of the wing.
VIEW Step 2: Calculate the twist angle.
VIEW Step 3: Find the reactions at the fixed end.
VIEW Step 4: Find the shear modulus, the polar moment of inertia, and the angular deflection.
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