By James Palmer, K.W. Ramsden, E.M. Goodger
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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
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.
82660 1. 84029 1. 84695 1. 710 0. 77202 0. 00351 1. 88581 0. 76735 1. 75861 1. 550 T/T* t/t* pjp* P/P* V/V* 1. 72362 1. 765 o. 770 0.
88581 0. 76735 1. 75861 1. 550 T/T* t/t* pjp* P/P* V/V* 1. 72362 1. 765 o. 770 0.