A gas of standard temperature and pressure (STP) has a mass of 1,1 kg. The gas undergoes an isothermal process to 780 kPa. Take the specific heat capacity at constant pressure as 1,005 kJ/kg.K and the specific heat capacity at constant volume as 0,717 kJ/kg.K

Calculate the following:
2.1
The characteristic gas constant in kJ/kg.K
2.2
The density at STP

1 answer

To solve the given problems, we need to use some fundamental equations related to ideal gases and specific heat capacities.

2.1: Characteristic Gas Constant

The characteristic gas constant \( R \) can be calculated using the specific heat capacities at constant pressure \( C_p \) and at constant volume \( C_v \). The relationship is given by:

\[ R = C_p - C_v \]

Where:

  • \( C_p = 1.005 \text{ kJ/kg.K} \)
  • \( C_v = 0.717 \text{ kJ/kg.K} \)

Now, plugging in the values:

\[ R = 1.005 - 0.717 = 0.288 \text{ kJ/kg.K} \]

Result of 2.1:

The characteristic gas constant \( R \) is 0.288 kJ/kg.K.


2.2: Density at STP

To calculate the density of the gas at Standard Temperature and Pressure (STP), we can use the Ideal Gas Law:

\[ PV = nRT \]

Where:

  • \( P \) is the pressure,
  • \( V \) is the volume,
  • \( n \) is the number of moles,
  • \( R \) is the specific gas constant, and
  • \( T \) is the temperature in Kelvin.

At STP:

  • Standard Pressure \( P = 101.325 \text{ kPa} \)
  • Standard Temperature \( T = 273.15 \text{ K} \)

We need to calculate the density \( \rho \), which is given by:

\[ \rho = \frac{mass}{volume} = \frac{m}{V} \]

We can also express volume in terms of pressure, number of moles, and the specific gas constant:

From the ideal gas equation, we rearrange to find \( V \):

\[ V = \frac{nRT}{P} \]

The number of moles \( n \) can be expressed as:

\[ n = \frac{m}{M} \]

Where \( M \) is the molar mass. However, we don't need the exact value of \( M \) to find density if we can express \( \rho \) in terms of \( m \) and \( R \):

At STP, substituting the values into the density equation yields:

Using the equation \( PV = \rho RT \), we can rearrange to find:

\[ \rho = \frac{P}{RT} \]

Now substituting in the known values:

\[ \rho = \frac{101.325 \text{ kPa}}{0.288 \text{ kJ/kg.K} \times 273.15 \text{ K}} \]

Note: Convert 101.325 kPa to kJ, where \( 1 \text{ kPa} = 0.001 \text{ MPa} = 0.001 \text{ kJ/L} \):

\[ \rho = \frac{101.325 \times 0.001 \text{ kJ}}{(0.288) \times 273.15} \]

Calculating this gives:

\[ \rho \approx \frac{0.101325}{0.0786} \approx 1.292 \text{ kg/m}^3 \]

Result of 2.2:

The density at STP is approximately 1.292 kg/m³.

These results can be useful in various applications related to gases and thermodynamics.