A plane is in level flight at constant speed and each of its two wings
has an area of 25 m². If the speed of air is 180 km/h over the lower
(b)
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The area of the wings of the plane, A=2×25=50sq−m
Speed of air over the lower wing, V
1
=180km/h=50m/s
Speed of air over the upper wing, V
2
=234km/h=65m/s
Density of air, =1kg/cu.m
Pressure of air over the lower wing =P
1
Pressure of air over the upper wing =P
2
The upward force on the plane can be obtained using Bernoullis equation as:
P
1
−P
2
=
2
1
ρ(V
2
2
−V
1
2
)
F=(P
1
−P
2
)A=
2
1
ρ(V
2
2
−V
1
2
)A
F=(P
1
−P
2
)A=
2
1
×1×(65
2
−50
2
)×50=43125N
∴m=
g
F
=4400kg
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