Answer:
<em>a) 42 mm</em>
<em>b) 144.4 MPa</em>
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Explanation:
Load P = 200 kN = 200 x 10^3 N
Torque T = 1.5 kN-m = 1.5 x 10^3 N-m
maximum shear stress τ = 100 Mpa = 100 x 10^6 Pa
diameter of shaft d = ?
From T = τ *
* 
substituting values, we have
1.5 x 10^3 = 100 x 10^6 x
x 
= 7.638 x 10^-5
d =
= 0.042 m = <em>42 mm</em>
b) Normal stress = P/A
where A is the area
A =
=
= 1.385 x 10^-3
Normal stress = (200 x 10^3)/(1.385 x 10^-3) = 144.4 x 10^6 Pa = <em>144.4 MPa</em>
Answer:
438.4$ each month
Explanation:
you get this answer by dividing the total payment by the months
Explanation:
uuui ielts k oshru with the best of my life u
Answer:
1) This is because too much fuel is needed to get a payload from the surface to orbital altitude an accelerated to orbital speed.
2) This is because space travel present extreme environment that affect machines operations and survival.
Explanation:
Hope it helps