Aerospace Engineering > GATE 2022 > Pressure Calculation
A rotational velocity field in an air flow is given as V⃗ = ayî + bxĵ, with a = 10 s-1, b = 20 s-1.
The air density is 1.0 kg/m3 and the pressure at (x, y) = (0 m, 0 m) is 100 kPa.
Neglecting gravity, the pressure at (x, y) = (6 m, 8 m) is _______ kPa. (rounded off to nearest integer)

Correct : 88 to 91

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rotational velocity field fluid dynamics pressure aerospace engineering GATE 2022 GATE AE 2022 Q50 pressure calculation fluid flow incompressible flow Euler's equation fluid mechanics aerodynamics pressure

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