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Kerne method

This compares to assumed value of 0.001 + 0.001 = 0.002 The Kern method is usually easier to handle for pressure systems than for vacuum systems. The recirculation ratio is higher and, therefore, requires more trials to narrow-in on a reasonable value for the low pressure systems. The omission of two-phase flow in pressure drop analysis may be a serious problem in the low pressure system, because a ratio on the high side may result, causing a high hj value. In general, however, for systems from atmospheric pressure and above, the method usually gives conservative results when used within Kern s limitations. [Pg.202]

The design calculations highlighted the shortcomings of the Kern method of exchanger design. The Kern method fails to account for shell-side inefficiencies such as bypassing, leakage, crossflow losses, and window losses. This leads to a marked overestimate of the shell-side heat-transfer coefficient and shell-side pressure drop. The Bell method is recommended to correct these deficiencies. [Pg.191]

The shell-side heat-transfer coefficient in the Kern method is calculated using Equation 10.2. An equivalent diameter is calculated which is representative of the shell-side fluid passage geometry. Equation 10.2 therefore becomes ... [Pg.194]

The Kern method is inaccurate for calculating the shell-side heat-transfer coefficient and shell-side pressure drop (Ref. E2, p. 545). Kern makes no account of the effect of bypss and leakage in the shell-fluid passage. For these reasons the Bell Method (Ref. E9) is employed to serve as a check on the preliminary design. [Pg.195]

The other parameter also needing revision was the shell-side pressure drop. This was reduced from 50 kPa (Kern method) to around 6 kPa. The Kern method is subject to overestimates of the pressure drop for the reasons already discussed. [Pg.204]

H.4 Tube-side Heat-transfer Coefficient (The Kern method) 314 H.5 Shell-side Heat-transfer Coefficient (The Kern method) 315 H.6 Overall Heat-transfer Coefficient 316... [Pg.226]

H.7 Tube-side Pressure Drop (The Kern Method) 317... [Pg.226]

H.4 Tube-side Heat-transfer Coefficient (The Kern Method)... [Pg.314]

This design based upon the Kern method appears to be quite adequate, on the basis of the results obtained. [Pg.318]

This value is obviously much lower than that calculated by the Kern method. This means that the previously calculated value for the overall heat-transfer coefficient must also be revised. [Pg.321]


See other pages where Kerne method is mentioned: [Pg.695]    [Pg.428]    [Pg.193]    [Pg.193]    [Pg.196]    [Pg.204]    [Pg.318]    [Pg.359]    [Pg.141]   
See also in sourсe #XX -- [ Pg.186 , Pg.491 ]




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