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Question

Air enters a 28 cm diameter pipe steadily at 200 kPa and 20°C with a velocity of 5 m/s. Air is heated as it flows and leaves the pipe at 180 kPa and 40°C. The mass flow rate of air is (take Gas constant, R, for air, as 0.287 kJ/kg.K)

The correct answer is

0.7318 kg/s

Calculating Air Mass Flow Rate in a Pipe

The question asks for the mass flow rate of air entering a pipe under steady flow conditions. To find the mass flow rate ($\dot{m}$), we need the density of the air at the inlet ($\rho_1$), the cross-sectional area of the pipe ($A$), and the inlet velocity ($V_1$). The formula for mass flow rate is:

\(\dot{m} = \rho_1 \times A \times V_1\)

First, let's list the given information and convert units to be consistent with SI units (meters, kilograms, seconds, Kelvin, Pascals, Joules):

  • Pipe diameter, $D = 28 \text{ cm} = 0.28 \text{ m}$
  • Inlet pressure, $P_1 = 200 \text{ kPa} = 200 \times 10^3 \text{ Pa}$
  • Inlet temperature, $T_1 = 20^\circ\text{C}$. We need to convert this to Kelvin: \(T_1 = 20 + 273.15 = 293.15 \text{ K}\).
  • Inlet velocity, $V_1 = 5 \text{ m/s}$
  • Gas constant for air, $R = 0.287 \text{ kJ/kg.K} = 0.287 \times 10^3 \text{ J/kg.K}$

Note that the outlet conditions ($P_2$ and $T_2$) are given, but for calculating the mass flow rate *at the inlet*, we only need the inlet conditions and the gas constant, since the mass flow rate is constant in steady flow.

Next, we need to calculate the cross-sectional area of the pipe. Since the pipe is circular, the area is given by:

\(A = \frac{\pi D^2}{4}\)

Substituting the diameter:

\(A = \frac{\pi (0.28 \text{ m})^2}{4} \approx \frac{3.14159 \times 0.0784 \text{ m}^2}{4} \approx 0.061575 \text{ m}^2\)

Now, we need to find the density of air at the inlet conditions ($\rho_1$). We can use the ideal gas law, which states \(P V = m R T\). Dividing by volume \(V\) and rearranging gives \(P = \frac{m}{V} R T\). Since density \(\rho = \frac{m}{V}\), we have \(P = \rho R T\). We can solve for density:

\(\rho_1 = \frac{P_1}{R T_1}\)

Substituting the values (using consistent units):

\(\rho_1 = \frac{200 \times 10^3 \text{ Pa}}{(0.287 \times 10^3 \text{ J/kg.K}) \times (293.15 \text{ K})}\)

\(\rho_1 = \frac{200000}{287 \times 293.15} \text{ kg/m}^3\)

\(\rho_1 \approx \frac{200000}{84056.05} \text{ kg/m}^3\)

\(\rho_1 \approx 2.3793 \text{ kg/m}^3\)

Finally, we can calculate the mass flow rate using the formula \(\dot{m} = \rho_1 \times A \times V_1\):

\(\dot{m} = (2.3793 \text{ kg/m}^3) \times (0.061575 \text{ m}^2) \times (5 \text{ m/s})\)

\(\dot{m} \approx 0.7318 \text{ kg/s}\)

The calculated mass flow rate of air is approximately 0.7318 kg/s.

Let's compare this result with the given options:

  • 7.318 kg/s
  • 0.7318 kg/s
  • 0.3079 kg/s
  • 10.727 kg/s

Our calculated value matches one of the options.

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