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Entropy and Second Law of Thermodynamics

 

  • Equation (38.24) does not tell us about the direction (i.e., a hot body with respect to its surrounding will gain temperature or cool down) of the process. To determine the proper direction of a process, we define a new state variable, entropy, which is

                      Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                    (38.25)

where s is the entropy of the system,  δqrev is the heat added reversibly to the system and T is the temperature of the system. It may be mentioned that Eqn. (38.25) is valid if both external and internal irreversibilities are maintained during the process of heat addition

 

  • Entropy is a state variable and it can be associated with any type of process, reversible or irreversible. An effective value of δqrev can always be assigned to relate initial and end points of an irreversible process, where the actual amount of heat added is δq . One can write

                 Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                 (38.26)         

 

It states that the change in entropy during a process is equal to actual heat added divided by the temperature plus a contribution from the irreversible dissipative phenomena. It may be mentioned that dsirrev implies internal irreversibilities if T is the temperature at the system boundary. If T is the temperature of the surrounding dsirrev implies both external and internal irreversibilities. The irreversible phenomena always increases the entropy, hence       

 

                Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                         (38.27)   

  • Significance of greater than sign is understandable. The equal sign represents a reversible process. On combining Eqs (38.26) and (38.27) we get           

 

                     Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                          (38.28)                    

If the process is adiabatic, Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering, Eq. (38.28) yields 

                   Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                         (38.29)

  • Equations (38.28) and (38.29) are the expressions for the second law of thermodynamics. The second law tells us in what direction the process will take place. The direction of a process is such that the change in entropy of the system plus surrounding is always positive or zero (for a reversible adiabatic process). In conclusion, it can be said that the second law governs the direction of a natural process.    

 

  • For a reversible process, it can be said that  δW = - pdv where dv is change in volume and from the first law of thermodynamics it can be written as

    δq - pdv = de                                                 (38.30)                          

                              
  • If the process is reversible, we use the definition of entropy in the form  δqrev = Tds the Eq. (38.30) then becomes,
    δq - pdv = de
           Tds = de + pdv                                         (38.31)              

                   
  • Another form can be obtained in terms of enthalpy. For example, by definition

    h = e +pv

    Differentiating, we obtain

    dh = de + pdv + vdp                                  ( 38.32)                   

Combining Eqs (38.31) and (38.32), we have

                  Tds = dh + vdp                                  ( 38.33) 

  • Equations (38.31) and (38.33) are termed as first Tds equation and second Tds equation, respectively.
     
  • For a thermally perfect gas, we have dh= cpdt  (from Eq. 38.20) , substitute this in Eq. (38.33) to obtain

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                                  ( 38.34)                              

Further substitution of pv = RT into Eq. (38.34) yields

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                     ( 38.35) 

Integrating Eq. (38.35) between states 1 and 2,

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                  ( 38.36)       

 

If   cp  is a variable, we shall require gas tables; but for constant  cp  we obtain the analytic expression    

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                   ( 38.37)       



In a similar way, starting with Eq. (38.31) and making use of the relation  the change in entropy can also be written as

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                       ( 38.38)     

 

Isentropic Relation

An isentropic process is a reversible-adiabatic process. For an adiabatic process  δq = 0 and for a reversible process, dsirrev = 0 From Eq. (38.26), for an isentropic process, ds = 0 However, in Eq. (38.37), substitution of isentropic condition yields

  Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering              (38.39)

 

Using  Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering  , we have

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                      (38.40)

Considering Eq. (38.38), in a similar way, yields

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering                    (38.41)

 

Using      Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering      we get

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering           (38.42)

 

  • Using Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering we can write

 

               Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering              (38.43)

 

  • Combining Eq. (38.40) with Eq. (38.43), we find,

 

Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering       (38.44)
 

This is a key relation to be remembered throughout the chapter.

 

 

                       

The document Introduction to Compressible Flow - 2 | Fluid Mechanics for Mechanical Engineering is a part of the Mechanical Engineering Course Fluid Mechanics for Mechanical Engineering.
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FAQs on Introduction to Compressible Flow - 2 - Fluid Mechanics for Mechanical Engineering

1. What is compressible flow in mechanical engineering?
Ans. Compressible flow refers to the flow of a fluid, such as gas or air, where the density changes significantly due to variations in pressure and temperature. In mechanical engineering, it is important to understand compressible flow as it affects the performance and design of various systems, such as gas turbines, jet engines, and compressors.
2. How is compressible flow different from incompressible flow?
Ans. Compressible flow and incompressible flow are two distinct types of fluid flow. In compressible flow, the density of the fluid changes significantly, and the flow behavior is influenced by variations in pressure and temperature. On the other hand, in incompressible flow, the density remains nearly constant, and the flow behavior is primarily determined by changes in velocity and viscosity.
3. What are the key parameters that affect compressible flow?
Ans. Several parameters influence compressible flow, including Mach number, Reynolds number, and specific heat ratio. The Mach number represents the ratio of the flow velocity to the speed of sound and determines whether the flow is subsonic, transonic, or supersonic. The Reynolds number relates to the flow's inertia and viscosity, while the specific heat ratio characterizes the thermodynamic properties of the fluid.
4. How is compressible flow analyzed and calculated in mechanical engineering?
Ans. Compressible flow is analyzed using various equations and principles, such as the conservation of mass, momentum, and energy. The continuity equation, Euler's equation, and the energy equation (Bernoulli's equation) are commonly employed to calculate the flow properties, including velocity, pressure, and temperature. Additionally, specialized software and computational fluid dynamics (CFD) techniques are often utilized for detailed analysis and simulations.
5. What are some practical applications of compressible flow in mechanical engineering?
Ans. Compressible flow has numerous practical applications in mechanical engineering. It is crucial in the design and analysis of gas turbine engines, where the compression and expansion of air play a vital role in generating power. Compressible flow is also significant in the design of supersonic aircraft, rocket engines, and high-speed wind tunnels. Additionally, it is essential in the design of piping systems, compressors, and ventilation systems that involve the flow of gases.
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