Calculate the mass (in metric tons) of a blade made of Aluminum, M_{blade}^{Al}M
blade
Al
, setting the stress limit equal to fatigue limit of the material, \sigma_0^{Al} = 150 MPaσ
0
Al
=150MPa.
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Hence the value of M = 2 x (Ao ^flap + A0 ^edge) x 86 x 2700 = M / 1000 in tons.
Explanation:
We need to calculate this first:
- Ao^flap = 81 x 8π x σo^flap x ho^flap x ρ (air) x V x r^2 x L^3
- σo^flap = 150 x 10^6
- Then calculate Ao^edge
- σo^edge = 150 x 10^6
- Then find the value of M
- M = 2 x (Ao ^flap + A0 ^edge) x 86 x 2700
- Hence the value of M = 2 x (Ao ^flap + A0 ^edge) x 86 x 2700 = M / 1000 in tons.
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