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A two-fluid model for refrigerant flow through adiabatic capillary tubes

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Abstract

This work presents a numerical model to simulate refrigerant flow through capillary tubes, commonly used as expansion devices in refrigeration systems. The flow is divided in a single-phase region, where the refrigerant is in the subcooled liquid state, and a region of two-phase flow. The capillary tube is considered straight and horizontal. The flow is taken as one-dimensional and adiabatic. Steady-state condition is also assumed and the metastable flow phenomena are neglected. The two-fluid model, considering the hydrodynamic and thermal non-equilibrium between the liquid and vapor phases, is applied to the two-phase flow region. Comparisons are made with experimental measurements of the mass flow rate and pressure distribution along two capillary tubes working with refrigerant R-134a in different operating conditions. The results indicate that the present model provides a better estimation than the commonly employed homogeneous model. Some computational results referring to the quality, void fraction, velocities, and temperatures of each phase are presented and discussed.

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Abbreviations

A :

Cross-sectional area of the tube, m2

A d :

Surface area of the suspended particle, m2

a i :

Interfacial area per unit volume, 1/m

B d :

Volume of the suspended particle, m3

C mv :

Virtual mass coefficient

C fi :

Interfacial friction coefficient

C D :

Drag coefficient

C r :

Relaxation coefficient

C :

Velocity of sound, m/s

c p :

Specific heat capacity, J/(kg/K)

D :

Internal diameter of the tube, m

D C :

Internal diameter of inlet device, m

d :

Mean bubble diameter, m

d 0 :

Initial mean bubble diameter, m

F LV :

Interfacial force per unit volume, N/m3

F mv :

Virtual mass force per unit volume, N/m3

F wk :

Wall friction force per unit volume to phase k, N/m3

f :

Friction factor

f B :

Two-phase flow region friction factor

G :

Mass flux, kg/(m2 s)

h :

Specific enthalpy, J/kg

\( \hat{h}_{i} \) :

Interfacial heat transfer coefficient, W/mK

K :

Pressure loss factor associated with the inlet device

\( \hat{k} \) :

Thermal conductivity, W/(mk)

L :

Tube length, m

M :

Mach number

\( \dot{m} \) :

Refrigerant mass flow rate, kg/s

N :

Bubble number density, 1/m3

Pr :

Prandtl number

p :

Pressure, N/m2

q i :

Interfacial heat flux, W/m2

Re :

Reynolds number

S 0 :

Initial slip between the phases

T :

Temperature, K

V :

Specific volume, m3/kg

V :

Velocity, m/s

x :

Vapor mass fraction (quality)

z :

Axial distance, m

α :

Superficial void fraction

Γ :

Interfacial mass flux per unit volume, kg/(ms)

ΔT sub :

Subcooling, K

ε :

Tube wall roughness, μm

η :

Wallis parameter for momentum flux due to phase change

µ :

Dynamic viscosity, kg/(m s)

ρ :

Density, kg/m3

k = L, V:

Phase index, liquid and vapor respectively

i:

Interface

sat:

Saturation state

ent:

Capillary tube inlet

o:

Initial values

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Acknowledgments

This work was performed under a technical and scientific cooperation agreement between the Research Laboratories for Emerging Technologies in Cooling and Thermophysics of the Department of Mechanical Engineering of Federal University of Santa Catarina and EMBRACO. The support received from EMBRACO during the many stages of this research is gratefully acknowledged, with special recognition to Eng. José Lainor Driessen and Eng. Roberto Horn Pereira for their encouragement and assistance. Thanks also goes to Dr. Jader Riso Barbosa Jr. who helped during the preparation of the final version of this work.

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Correspondence to André Luiz Seixlack.

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Technical Editor: Jose Parise.

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Seixlack, A.L., Prata, Á.T. & Melo, C. A two-fluid model for refrigerant flow through adiabatic capillary tubes. J Braz. Soc. Mech. Sci. Eng. 36, 1–12 (2014). https://doi.org/10.1007/s40430-013-0051-9

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