Q6. An aircraft (\( m = 2.5 \times 10^5 \, \text{kg} \), wing area \( 400 \, \text{m}^2 \)) flies at \( 900 \, \text{km/h} \). What is the pressure difference across the wings? (Take \( g = 10 \, \text{m/s}^2 \), \( \rho_{\text{air}} = 1.2 \, \text{kg/m}^3 \))
- A. 5000 Pa
- B. 6250 Pa
- C. 7500 Pa
- D. 8750 Pa