MCQMediumJEE 2023Bernoulli's Theorem

JEE Physics 2023 Question with Solution

A fully loaded Boeing aircraft has a mass of 5.4×105kg5.4 \times 10^5 \, \text{kg}. Its total wing area is 500m2500 \, \text{m}^2. It is in level flight with a speed of 1080km/h1080 \, \text{km/h}. If the density of air (ρ\rho) is 1.2kg/m31.2 \, \text{kg/m}^3, the fractional increase in the speed of the air on the upper surface of the wing relative to the lower surface in percentage will be (g=10m/s2g = 10 \, \text{m/s}^2):

  • A

    16%16\%

  • B

    6%6\%

  • C

    8%8\%

  • D

    10%10\%

Answer

Correct answer:D

Step-by-step solution

Standard Method

Given: mass of aircraft =5.4×105kg= 5.4 \times 10^5 \, \text{kg}, wing area =500m2= 500 \, \text{m}^2, speed =1080km/h=300m/s= 1080 \, \text{km/h} = 300 \, \text{m/s}, air density =1.2kg/m3= 1.2 \, \text{kg/m}^3, and g=10m/s2g = 10 \, \text{m/s}^2.

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

(P2P1)A=mg(P_2 - P_1)A = mg

Hence,

P2P1=5.4×105×10500=10.8×103N/m2P_2 - P_1 = \frac{5.4 \times 10^5 \times 10}{500} = 10.8 \times 10^3 \, \text{N/m}^2

Using Bernoulli’s principle,

P2P1=12ρ(V12V22)=ρ(V1V2)(V1+V2)P_2 - P_1 = \frac{1}{2}\rho (V_1^2 - V_2^2) = \rho (V_1 - V_2)(V_1 + V_2)

Substituting the given values,

10.8×103=1.2×(V1V2)×60010.8 \times 10^3 = 1.2 \times (V_1 - V_2) \times 600

So,

V1V2=30m/sV_1 - V_2 = 30 \, \text{m/s}

Therefore,

V1V2V1×100=30300×100=10%\frac{V_1 - V_2}{V_1} \times 100 = \frac{30}{300} \times 100 = 10\%

Therefore, the fractional increase in speed is 10%10\%. The correct option is D. The solution marks B, but the extracted working gives 10%10\%, which matches option D.

Common mistakes

  • Using the marked answer B without checking the working. Here the solution label conflicts with the calculation. The worked steps give 10%10\%, so the derivation must be trusted over the listed letter.

  • Forgetting to convert 1080km/h1080 \, \text{km/h} into 300m/s300 \, \text{m/s}. Bernoulli’s equation must be used in SI units, otherwise the percentage change becomes incorrect.

  • Taking lift force directly as pressure difference without multiplying by wing area. The correct relation is ΔPA=mg\Delta P \cdot A = mg, so area must be included before applying Bernoulli’s principle.

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