By James Palmer, K.W. Ramsden, E.M. Goodger
Read Online or Download Compressible Flow Tables for Engineers: With Appropriate Computer Programs, for Estimating Property Changes Caused by Friction Heat Transfer and/or Shock Waves PDF
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Additional info for Compressible Flow Tables for Engineers: With Appropriate Computer Programs, for Estimating Property Changes Caused by Friction Heat Transfer and/or Shock Waves
76273 1. 75236 2. 22330 2. Isothermal Flow (Isothermal constant area flow with friction) Introduction These data are applicable to the transport of gas over very long distances. Although the Mach Number is usually quite low, large changes in pressure occur, so that the compressibility of the fluid cannot be ignored. For fairly short parallel ducts the assumption of an adiabatic flow is more appropriate (see page 65). 250. Note Values of the friction factor Cr are given by L. F. Moody in 'Friction Factors for Pipe Flow', Trans.
2 . /G WRITE(6,3) 3 FORMAT(/' Enter min. M, increment of M & max. ,O. O. O •. (50*(N/50))))WRITE(2,4)GAMMA 4 FORMAT(//14X, 'ISarHERMAL FLCM' / /14X, 'GAMMA = ', FS. 04948 0. 01283 5. 77932 o. 80064 1. 77741 1. 75491 1. 54856 1. 47466 1. 86187 1. 71554 o. 765 0. 770 0. 02314 3. Rayleigh Flow (Frictionless constant area flow with heat exchange) Introduction The assumptions implicit in simple heating or cooling (Rayleigh flow) lead to less accurate solutions to real problems met in practice than for other types of flow covered in this book.
Similarly, internal heat transfer through conventional combustion of fuel gases and vapours will change gas composition. However, if the temperature difference between the flowing gas and the duct walls is large, the effects on property changes due to friction and/or gas composition will be secondary. Accordingly, the assumption of simple heating or cooling provides a useful estimate of relevant property changes. These data are applicable to approximate calculations in parallel flow when the effects of friction can be ignored.