Given: mass of aircraft =5.4×105kg, wing area =500m2, speed =1080km/h=300m/s, air density =1.2kg/m3, and g=10m/s2.
Find: the fractional increase in air speed on the upper surface relative to the lower surface, in percentage.
In level flight, the lift balances the weight, so
(P2−P1)A=mg
Hence,
P2−P1=5005.4×105×10=10.8×103N/m2
Using Bernoulli’s principle,
P2−P1=21ρ(V12−V22)=ρ(V1−V2)(V1+V2)
Substituting the given values,
10.8×103=1.2×(V1−V2)×600
So,
V1−V2=30m/s
Therefore,
V1V1−V2×100=30030×100=10%
Therefore, the fractional increase in speed is 10%. The correct option is D. The solution marks B, but the extracted working gives 10%, which matches option D.