Air enters the 1 m² inlet of an aircraft engine at 100 kPa and 20° C with a velocity of 180 m/s. Determine: a) The volumetric flow rate in m^3/s b) The mass flow rate kg/s Assume air to be an ideal gas

Respuesta :

Answer:

a) 180 m³/s

b) 213.4 kg/s

Explanation:

[tex]A_1[/tex] = 1 m²

[tex]P_1[/tex] = 100 kPa

[tex]V_1[/tex] = 180 m/s

Flow rate

[tex]Q=A_1V_1\\\Rightarrow Q=1\times 180\\\Rightarrow Q=180\ m^3/s[/tex]

Volumetric flow rate = 180 m³/s

Mass flow rate

[tex]\dot{m}=\rho Q\\\Rightarrow \dot m=\frac{P_1}{RT} Q\\\Rightarrow \dot m=\frac{100000}{287\times 293.15}\times 180\\\Rightarrow \dotm=213.94\ kg/s[/tex]

Mass flow rate = 213.4 kg/s

The volumetric flow rate and mass flow rate are respectively; Q₁ = 180 m³/s and m' = 213.4 kg/s

What is Volumetric and Mass Flow rate?

We are given;

Initial cross sectional area; A₁ = 1 m²

The inlet pressure of the air; P₁ = 100 kPa = 100000 Pa

The inlet velocity; V₁ = 180 m/s

Inlet Temperature; T₁ = 20 °C = 293.15 K

A) Formula for Volumetric rate is;

Q₁ = A₁ * V₁

Q₁ = 1 * 180

Q₁ = 180 m³/s

B) Formula for mass flow rate is;

m' = PQ/RT

where R = 287 J/kg.k

Thus;

m' = (100000 * 180)/(287 * 293.15)

m' = 213.4 kg/s

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