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158                                            Part II Gas Drilling Systems


        sound in the fluid under the in situ condition, the flow is called a sonic
        flow. Under a sonic flow condition, the pressure wave downstream of
        the orifice cannot propagate upstream through the orifice because the
        medium (fluid) is traveling in the opposite direction at the same or higher
        velocity. This causes a pressure discontinuity at the orifice—that is, the
        upstream pressure is not influenced by the downstream pressure.
           A sonic flow can have many harmful effects on gas drilling operations,
        including pipes sticking, ice/hydrate balling of bits, wellbore washouts, and
        crooked holes. Because of the pressure discontinuity at the orifice, any
        increase in bottomhole pressure due to cuttings accumulation or mud ringing
        in the annulus cannot be detected by reading the standpipe pressure gauge.
        Cuttings will continue to accumulate until the drill string gets stuck. Often
        pipe sticking occurs only a few minutes after a “smooth” drilling operation.
        The operation looked smooth because the standpipe pressure was normal,
        while the annular pressure had already increased due to cuttings accumulation
        or mud ringing. To reduce the possibility of pipe sticking, sonic flow should
        be avoided by using larger bit nozzles or orifices in all gas drilling operations.
           Whether sonic flow exists at the bit depends on the downstream–
        upstream pressure ratio. If this pressure ratio is less than a critical pressure
        ratio, sonic flow exists. The critical pressure ratio depends on the fluid
        properties, not on the configuration of the orifice. It is expressed as
                                                k
                                               k−1
                                      =                              (7.7)
                                 P dn      2
                                 P up     k + 1
                                    c
        Since the values of the specific heat ratio (k) of air and natural gases are
        between 1.2 and 1.4, Eq. (7.7) gives the critical pressure ratio values ranging
        from 0.51 to 0.53. Use of these numbers in Eq. (7.6) shows an 84% reduc-
        tion in the absolute temperature scale and more reduction in the relative
        temperature scale (°For °C).
           Under sonic flow conditions the upstream pressure is given by the
        following equation for ideal gases:
                                         v ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
                                         u    S g T up
                                   Q g
                           P up =        u                           (7.8)
                                         u          k + 1
                                609:33A o  u       k−1
                                               2
                                           k
                                         t
                                              k + 1
        where
           Q g = gas flow rate, scf/min or scm/min
                                       2     2
           A o = total area of bit orifices, in or m
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