Page 271 - Air and Gas Drilling Manual
P. 271

6-16    Air and Gas Drilling Manual
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                                                     37 .
                                        f  =−  2 log           D e i     +  N 251 f        (6-47)
                                                              R
                                                                 
                                                                 
                               where e is  the absolute roughness of the inside surface of  the  drill  string  (ft).    In
                               general, Equation 6-47 is valid for values of Reynolds numbers from 2,000 to 4,000.
                                   The  empirical  expression  for  the  Fanning  friction  factor  for  turbulent  flow
                               conditions is known as the von Karman equation.  This empirical expression is
                                                            2
                                                           
                                                  1        
                                      f =                                            (6-48)
                                                  D 
                                                
                                           2 log.          
                                                   i
                                                      + 1 14
                                                  e    
                                                           
                               In general, Equation 6-48 is valid for values of Reynolds numbers greater than 4,000.
                                   For follow-on calculations for flow in the drill string the absolute roughness for
                               commercial pipe, e p =  0.00015  ft,  will  be used for the inside  surfaces  of  the  drill
                               pipe and drill collars.
                                   Equation  6-45  together  with  Equations  6-46  through  6-48  can  be  used  in
                               sequential integration steps starting at the bottom  of  the  inside  of  the  drill  string
                               (with the known pressure above the drill  bit  inside the drill  string) and continuing
                               for each subsequent change in  cross-sectional  area  inside  the  drill  string  until  the
                               injection pressure is  determined. These sequential calculation steps require trial and
                               error solutions.  The trial and error process requires the selection of the upper limit
                               of the pressure in each integral on the right side of Equation 6-44.   This  upper limit
                               pressure selection must  give a right side integral solution  that  is  equal  to  the  left
                               side integral solution.
                                   6.3  Air  and  Gas  Drilling  Model
                                   Air (or gas) drilling is a special case of the theory derived in  Section 6.2  above.
                               The  governing  equations  for  air  (or  gas)  drilling  operations  can  be  obtained  by
                               setting Q m = 0 in the equations derived in Section 6.2.
                                   There is two phase flow in the annulus (gas and rock cuttings).    Setting  Q m =  0
                               in Equation 6-25 yields

                                                         
                                                         
                                                 w ˙     
                                      dP =        t      
                                               P    T av    
                                              g
                                                    Q g 
                                               P    T    
                                                    g
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