Answer:
(a) The area of the duct exit is 1.67 m²
(b) The air pressure at the exit is 1.195 x 10⁵ N/m²
Step-by-step explanation:
Given;
inlet area, A₁ = 5 m²
inlet velocity, V₁ = 10 m/s
exit velocity, V₂ = 30 m/s
(a) The area of the duct exit is determined by applying continuity equation;
A₁V₁ = A₂V₂
Where;
A₂ is the area of the duct exit
A₂ = (A₁V₁) / (V₂)
A₂ = (5 x 10) / (30)
A₂ = 1.67 m²
(b) Apply Bernoulli’s equation to determine the pressure at the exit;
![P_1 + (\rho V_1^2)/(2) = P_2 + (\rho V_2^2)/(2)\\\\P_2 = P_1 + (\rho V_1^2)/(2) - (\rho V_2^2)/(2)\\\\P_2 = P_1 + (\rho )/(2) (V_1^2 - V_2^2)](https://img.qammunity.org/2021/formulas/engineering/college/48o7466cu0kvyae6bhakssjcmg4ic3f90v.png)
Density of air at 300k = 1.177 kg/m³
![P_2 = P_1 + (\rho )/(2) (V_1^2 - V_2^2)\\\\P_2 = 1.2*10^5 \ + \ (1.177)/(2) (10^2 - 30^2)\\\\P_2 = 1.2*10^5 \ + \ -470.8\\\\P_2 = 1.195*10^5 \ N/m^2](https://img.qammunity.org/2021/formulas/engineering/college/zfeo9pxjpj35nekgikgi0damm8y1uvkm4x.png)
Therefore, the air pressure at the exit is 1.195 x 10⁵ N/m²