Page 132 - DJJ20063- Thermodynamics 1
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DJJ20063- Thermodynamics 1



                              Often C1 is negligible compared with C2. In this case the equation becomes

                                                      C  2   
                                                    +
                                     0  = m   (h  − h  )   2   
                                                      
                                                           
                                             2   1     2    
                                           
                                     C  2
                              or       2  =  (h −  h 2  )
                                             1
                                      2

                              or     C =     ( 2 h − h 2  )                                                        (3.30)
                                               1
                                       2

                      Example 3.8


                        Fluid with a specific enthalpy of 2800 kJ/kg enters a horizontal nozzle with negligible

                        velocity at the rate of 14 kg/s. At the outlet from the nozzle the specific enthalpy and

                                                                            3
                        specific volume of the fluid are 2250 kJ/kg and 1.25 m /kg respectively. Assuming an

                        adiabatic flow, determine the required outlet area of the nozzle.




                      Solution to Example 3.8
                      The steady flow energy equation gives



                                                   C  2  −C 2            
                                                  +
                              Q  −W  = m   (h 2  − h 1 )   2  1     ( + gZ 2  − gZ 1  )
                                                                            
                                                   
                                                      2                  
                                        
                                                                            

                      When applied to the nozzle, this becomes


                                              C  2  −C 2   
                                             +
                                     h
                              0 = m   ( − h 1 )    2  1   
                                                        
                                      2
                                                 2       
                                   

                      Since the inlet C1 is negligible, this may be written as
                                2
                              C =     ( 2 h − h  )
                                2       1   2
                                 C2   = √ [2(2800 – 22500]

                                    = √ 1100
                                    = 33.167 m/s


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