Source Models Vapor flow through holes and pipes Vapor flow though holes & pipes Vapor flow through holes Steady flow of vapor through pipes Example Liquid versus Vapor flow Liquids – Incompressible flow Vapors – Compressible flow Kinetic energy term is negligible Physical properties (density) constant Energy from pressure converted to kinetic energy Temperature, pressure, density all change when going through a hole or down a pipe Vapor flow though holes & pipes Vapor flow through holes Throttling release Free Expansion Non choked or subsonic Choked, critical or sonic Steady flow of vapor through pipes Example Vapor flow through holes Throttling flow Small cracks – large frictional loses Not much energy due to pressure is converted to kinetic Models require detailed information on physical structure of leak Throttling flow A throttling device is a valve or crack or porous material with high resistance to flow that results in a large pressure drop. Throttling flow First law of thermodynamics dE Q Ws min (h e p ek )in mout (h e p ek )out dt Assume Steady state Adiabatic Negligible potential and Kinetic energy effects Single inlet and outlet No shaft work Throttling flow Hence the process is isenthalpic Consider the temperature as a function of pressure and enthalpy dT fT ( P, h) Throttling flow Take partial T T dT dP dh P h h P Definition of Joule-Thomsen coefficient T P h Throttling flow If isenthalpic then Integrate out T 0 h P out Tout Tin dP in Most gases have positive Joule-Thomsen coefficient so as pressure drops, temperature drops Vapor flow though holes & pipes Vapor flow through holes Throttling release Free Expansion Non choked or subsonic Choked, critical or sonic Steady flow of vapor through pipes Example Vapor flow through holes Free Expansion Assume Negligible potential (ΔZ=0) No shaft work Ws=0 Vapor flow through holes Mechanical Energy Balance u2 g Ws Z F m 2 gc gc dP Friction through “hole” is defined as before dP F C dP 2 1 Vapor flow through holes Need to have density as a function of pressure to solve integral – Assume isentropic flow Pv P constant Cp Cv Vapor flow through holes Substitute all into MEB and integrate You end up with velocity as function of several terms u f P, P0 , T0 , properties As before, mass flow rate from velocity Qm uA Vapor flow through holes Design equation for subsonic flow through holes Eq. 4-38 2 g c M P P Qm C0 AP0 RgT0 1 P0 P0 2 1 Vapor flow though holes & pipes Vapor flow through holes Throttling release Free Expansion Non choked or subsonic Choked, critical or sonic Steady flow of vapor through pipes Example Choked flow through holes As you lower the down stream pressure (or increase upstream pressure) the velocity increases until it reaches a critical velocity, the sonic velocity, or speed of sound. After that the velocity becomes independent of pressure. Downstream conditions no longer have an effect on velocity. Choked flow through holes For choked, critical or sonic flow u a ( SpeedOfSound ) g c RgT / M So at choked conditions Eq. 4-40 Q m choked gc M 2 C0 AP0 RgT0 1 1 1 For sharp edged orifice C0=0.61, Worst case scenario C0=1.0 Choked flow through holes Pchoked 2 1 P0 1 Gas Pchoked Monotonic ~1.67 0.487P0 Diatomic (air) ~1.40 0.528P0 Triatomic ~1.32 0.542P0 Vapor flow though holes & pipes Vapor flow through holes Steady flow of vapor through pipes Adiabatic flow of vapor through pipes Non choked flows Choked flows Isothermal flow of vapor through pipes Non choked flows Choked flows Example Vapor flow through pipes There are two cases which we can derive (with much work) relationships for flow of vapors through pipes Adiabatic – which assumes well insulated walls, no energy loss to surroundings Isothermal – which assumes constant wall temperature (submerged pipe) Vapor flow though holes & pipes Vapor flow through holes Steady flow of vapor through pipes Adiabatic flow of vapor through pipes Non choked flows Choked flows Isothermal flow of vapor through pipes Non choked flows Choked flows Example Adiabatic vapor flow in pipes For compressible flow it is best to work things out in terms of the Mach number, Ma. u Ma a Adiabatic vapor flow through pipes The book doesn’t even attempt to go through the derivations, just gives the equations. As before, we need to consider both nonchoked and choked flow. Adiabatic vapor flow through pipes For most problems you know L – length of pipe d – diameter of pipe T1, P1 – upstream temperature, pressure P2 – downstream pressure To get mass flow rate Qm (mass/time) from G, mass flux, (mass/area*time) use Qm=G*A Adiabatic non choked flows in pipes 1) Find pipe roughness from Table 4-1 2) Determine f from Eq. 4-27 1 d 4log 3.7 f 3) Determine T2 from Eq. 4-51 (trial & error) 4) Calculation G from Eq. 4-52 5) Calculate Reynolds number to verify Eq 427 is valid Adiabatic Choked flows in pipes 1) Find roughness from Table 4-1 2) Determine f from Eq 4-27 3) Determine Ma1 from Eq 4-57 (use 4-46 to get Y1) (usually trial & error) 4) Determine mass flux, Gchoked Eq. 4-56 5) Determine Pchoked from Eq 4-54 6) Double check Reynolds number Vapor flow though holes & pipes Vapor flow through holes Steady flow of vapor through pipes Adiabatic flow of vapor through pipes Isothermal flow of vapor through pipes Non choked flows Choked flows Example Isothermal non choked flows 1) 2) 3) 4) Find roughness from Table 4-1 Determine f from Eq. 4-27 Compute G from Eq. 4-63 Double check Reynolds number For isothermal non choked flow no need for trial and error, nice analytical equations Isothermal choked flows 1) Find roughness from Table 4-1 2) Find f from Eq. 4-27 3) Determine Ma1 from Eq. 4-71 (trial and error) 4) Determine G from Eq. 4-70 5) Double check the Reynolds number Vapor flow though holes & pipes Vapor flow through holes Steady flow of vapor through pipes Example