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Mechanical Properties of Fluids

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Question : 27 of 31
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A plane is in level flight at constant speed and each of its two wings has an area of 25 m225\text{ m}^2. If the speed of the air is 180 km h1180\text{ km h}^{-1} over the lower wing and 234 km h1234\text{ km h}^{-1} over the upper wing surface, determine the plane’s mass. (Take air density to be 1 kg m3)1\text{ kg m}^{-3}).
Solution:  
Here, v1=180 km h1=50 m s1,v_{1}=180\text{ km h}^{-1}=50\text{ m s}^{-1},
v2=234 km h1=65 m s1v_{2}=234\text{ km h}^{-1}=65\text{ m s}^{-1}
area of the each wing, A=25 m2A = 25\text{ m}^2
and density of air, r=1 kg m3r = 1\text{ kg m}^{-3}
According to Bernoulli’s theorem,
P1P2=12ρ(v22v12)P_{1}-P_{2}= \frac{1}{2}\rho(v_{2}^{2}-v_{1}^{2})
=12(652502)= \frac{1}{2}(65^{2}-50^{2})
=862.5 N m2=862.5\text{ N m}^{-2}
Now, upward lift from both the wings,
F=(P1P2)×2AF = (P_1 - P_2) \times 2A
=862.5×2×25 N= 862.5 \times 2 \times 25\text{ N}
Let M be the mass of the plane. As the plane is in level flight,F=MgF = Mg
or M=Fg=862.5×2×259.8M = \frac{F}{g} = \frac{862.5 \times 2 \times 25}{9.8}
=4.4×103 kg=4.4 \times 10^{3}\text{ kg}.
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