Cryogenic Flow in Corrugated Pipes 2nd CASA Day: April 23, 2009 Patricio Rosen
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Motivation Corrugated Pipes/Hoses Portable Flexible Several Application Areas LNG Transport Development of DTSE (Dual Tank Stirling Engine) Goal Describe and Predict Flow Behavior in Corrugated Hoses in an Efficient Way
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Preliminaries P ¡ = : ¢ f ½ v 4 R Darcy Weisbach Equation Straight Pipe Poiseuille Flow Non-straight Pipes? Roughness Actual Shape L R P 1 2 v z P 1 ¡ 2 = : ¢ L f ½ v z 4 R v z = 2 µ 1 ¡ r R ¶ R e : = 4 ½ v z ¹ f = 6 4 R e
Moody Diagram Experimental Results Moody Diagram Fully Turbulent Colebrook Equation
LNG Composite Hose Moody Prediction Taking corrugation as roughnes Measurements Water LNG f = . 4 5 f = . 5 8 Moody Diagram is a poor indicator for the friction factor Find a better Alternative (CFD) f = . 1 3
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Set up saves lots of computation time Fluid Flow Equations Assumptions Incompressible Flow Steady Flow Gravity negligible Isothermal Flow One-phase Cylindrical and Periodic Hose Fixed Wall No Swirl Cylindrical Symmetry Navier-Stokes v ¢ r = ¡ 1 ½ @ P + º h 2 i z Periodicity v ( R z ) ; = r L P + k Set up saves lots of computation time
Analytic Expression for DFF From continuity Rewrite z-momentum Using Divergence Theorem For Poiseuille Flow v ¢ r z = ( ) ¡ r ¢ ( v z ) = ¡ 1 ½ P e + º : ¢ P L : = i n ¡ o u t 1 j µ Z z d S ¹ @ v ¶ Pressure “Friction“ Skin “Friction“ f = 6 4 ¹ D ½ v R e : ¢ P L = 8 ¹ v R 2 :
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
CFD Navier Stokes f 8 Setting > = < : + f Discretization @ P r = ~ z + f Discretization Velocity Pressure
Navier Stokes Re=2.13 Re=213 Re=2713 Re=676
Validation Several Corrugations (Re=213.5)
Forces at Wall Re=213 Re=2713 Pressure and Viscous Forces scale with Re in Laminar Regime and Skin Friction Dominates
Same Friction Factor as for Straight Pipes in Laminar Regime
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
CFD k-e Turbulence Model Re=177 Re=843 Re=1.737e4 Re=3860
Several Periods Re=177 Re=847 Re=3860
At High Reynolds Numbers the Pressure Forces become Dominant
Friction Factor One Period Several Periods
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Conclusions Correct Prediction of the Friction Factor Problem Solved? (One phase, adiabatic flow) Problem Solved? Sensibility of Results (needs validation) Cryogenic Liquids not yet manageable Expensive computation time for dynamic flow computations 4 hours Computation (NS Example)
Outline Motivation Pipe Flow Preliminaries Fluid Flow Equations CFD Navier Stokes CFD k-e Turbulence Model Conclusions Further work
Towards a 1D Model v ( r ; ) = + ^ d z ( R v ) = ¡ 1 ½ P Z ^ r ; + ` º : = 1 ¡ ( ) Z r ; d A ¡ i n ¡ o u t P ( z ) = 1 j ¡ Z d A d z ( R 2 v ) = ¡ 1 ½ P Z ^ r ; + ` º · @ ¸
Thanks for your attention!
RANS
k-e Model Summary
FEM for Navier Stokes
Navier Stokes Weak Form