Page 187 - 48Fundamentals of Compressible Fluid Mechanics
P. 187

9.4. THE WORKING EQUATIONS                                 
    149






                 
 SQ
QUQ
Q

            The temperature is     b  Q^S Q        VS    Q0S Q       Q^S IUI  %
                           Q0S 
( I(V (/3 
 
 V3 (
                                 L
                                      b
                             b
                                                      I-V S%

                                                 V Q
Q
H
                            L H
             With the temperature the speed of sound can be calculated as
                                 L
                                               #
                                   b L  H Q0S 
(
                       b
                                               I(V S% 
 S V 1G
             The pressure at point 1 can be calculated as
                            F L H
                      G H


                                        # #
                                     IUS V %!(

                                  b
                                      b

                                   b   H QS Q ( 
 Q % I K
                                                     QS
                             b
                            H

             The density as a function of other properties at point 1 is

                                               #


                                                          F

                            b  % S I
                                              I(Q W
                                                     I
S
                              H

             The mass flow rate can be evaluated from equation (9.2)  F
                                     H

                                            #


                                    cb #
                                                (

                                             I-V S%
                                 L %(






                                     V
                                  #
         (b) First, a check weather the flow is shockless by comparing the flow resistance
                               #
                                           # #
                                     QS Q
            and the maximum possible resistance. From the table or by using the attached
                        H I
S (
                                             
 
 S V H Q0S 3
                                                              1G
                   7
            program , obtain the flowing  
   
  
        ]





                          QS


            and the conditions of the tube are  V S    I
S Q  Q^S        ]  QS V
                  
 SQ
QUQ
Q  I3 Q^S I% 
 V3  Q I% I
S 3 V Q %(
                                          QS Q
Q
                                W`XaZ [
                                    H

                                        # #
            Since QS %  I3 the flow is chocked and with a shock wave.
                                      V
                                                    H Q0S %
           7           Q0S
                                          Q0S Q
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