Question:

A cylindrical furnace has height (𝐻) and diameter (𝐷) both 1 m. It is maintained at a temperature of 360 K. The air gets heated inside the furnace at constant pressure π‘ƒπ‘Ž and its temperature becomes 𝑇 = 360 𝐾. The hot air with density 𝜌 rises up a vertical chimney of diameter 𝑑 = 0.1 m and height β„Ž = 9 m above the furnace and exits the chimney (see the figure). As a result, atmospheric air of density πœŒπ‘Ž = 1.2 kg mβˆ’3, pressure π‘ƒπ‘Ž and temperature π‘‡π‘Ž = 300 K enter the furnace. Assume air as an ideal gas, neglecting the variations in 𝜌 and 𝑇 inside the chimney and the furnace. Also, ignore the viscous effects. [Given: The acceleration due to gravity 𝑔 = 10 m sβˆ’2 and πœ‹ = 3.14] Considering the airflow to be streamlined, the steady mass flow rate of air exiting the chimney is _______ gm sβˆ’1.

Updated On: Dec 14, 2024
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Approach Solution - 1

Applying Bernoulli's theorem,
\(P_a+\frac{1}{2}\rho_aV^2=P_a+\rho gH+\frac{1}{2}\rho V^2\,\,\,\,...........(1)\)
Also, since PM = \(\rho\)RT
\(\rho_{a}\times300=\rho\times360\)
\(\Rightarrow \rho=1\,kg/m^3\,\,\,..........(2)\)
\(\frac{v^2}{2}(0.2)=1\times10\times1\)
\(\Rightarrow v=10\,\,m/s\)
Mass flow rate = \(V\times \frac{\pi D^2}{4}\times \rho=10\times\frac{3.14}{4}\times\,\,1 kg/s=7.85\,\,kg/s=7850\,gm/s\)
 
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Approach Solution -2

We're given:

  1. Gas constants R and M remain constant, so MR​ is constant (for constant pressure).
  2. The density of hot air inside the furnace is 1.2 kg/m3 at a temperature of 300K and pressure Pa​.
  3. The air heats up at a constant pressure Pa​.

Given the buoyant force applied on the hot air is Vg in the upward direction and the weight of the hot air is also Vg in the downward direction, the net force on the hot air is π‘‰π‘”βˆ’π‘‰π‘”

Let the acceleration of the hot air in the upward direction be π‘Ža, and the mass of the hot air be 𝑉V.

We have:

\(a = \frac{V_g - V_g}{V} = \frac{g - g}{1.2} = \frac{0.8 \, \text{m/s}^2}{1.2} = 0.67 \, \text{m/s}^2\)

Using the formula for velocity 𝑣v of the hot air when exiting the chimney:

\(v = 2gh\)

Given \(v=6m/s\), we can solve for h:
\(6 = \sqrt{2 \times 9.8 \times h}\)
\(36=19.6h\) 
\(h = \frac{36}{19.6} \quad h \approx 1.83 \, \text{m}\)

The mass flow rate is given by:

Mass flow rate=\(\frac{\rho Av}{1000}\)

Given 𝐴=1 m2, we can calculate:

Mass flow rate=\(1.2 \times 1 \times \frac{6 }{ 1000} = 0.0072 \, \text{kg/s} = 7.2 \, \text{g/s} = 72 \, \text{gm/s}\)

So, the mass flow rate is \(72g/s.\)

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Concepts Used:

Thermodynamics

Thermodynamics in physics is a branch that deals with heat, work and temperature, and their relation to energy, radiation and physical properties of matter.

Important Terms

System

A thermodynamic system is a specific portion of matter with a definite boundary on which our attention is focused. The system boundary may be real or imaginary, fixed or deformable.

There are three types of systems:

  • Isolated System – An isolated system cannot exchange both energy and mass with its surroundings. The universe is considered an isolated system.
  • Closed System – Across the boundary of the closed system, the transfer of energy takes place but the transfer of mass doesn’t take place. Refrigerators and compression of gas in the piston-cylinder assembly are examples of closed systems.
  • Open System – In an open system, the mass and energy both may be transferred between the system and surroundings. A steam turbine is an example of an open system.

Thermodynamic Process

A system undergoes a thermodynamic process when there is some energetic change within the system that is associated with changes in pressure, volume and internal energy.

There are four types of thermodynamic process that have their unique properties, and they are:

  • Adiabatic Process – A process in which no heat transfer takes place.
  • Isochoric Process – A thermodynamic process taking place at constant volume is known as the isochoric process.
  • Isobaric Process – A process in which no change in pressure occurs.
  • Isothermal Process – A process in which no change in temperature occurs.

Laws of Thermodynamics

Zeroth Law of Thermodynamics

The Zeroth law of thermodynamics states that if two bodies are individually in equilibrium with a separate third body, then the first two bodies are also in thermal equilibrium with each other.

First Law of Thermodynamics 

The First law of thermodynamics is a version of the law of conservation of energy, adapted for thermodynamic processes, distinguishing three kinds of transfer of energy, as heat, as thermodynamic work, and as energy associated with matter transfer, and relating them to a function of a body's state, called internal energy.

Second Law of Thermodynamics 

The Second law of thermodynamics is a physical law of thermodynamics about heat and loss in its conversion.

Third Law of Thermodynamics

Third law of thermodynamics states, regarding the properties of closed systems in thermodynamic equilibrium: The entropy of a system approaches a constant value when its temperature approaches absolute zero.