Heat Transfer Study of Direct Contact Condensation in the Presence of Noncondensable Gas

2002 ◽  
Author(s):  
Yiban Xu ◽  
Shripad T. Revankar ◽  
Mamoru Ishii
Keyword(s):  
Heat Transfer ◽  
Nusselt Number ◽  
Direct Contact ◽  
Bubble Formation ◽  
Density Ratio ◽  
Size Variation ◽  
Least Square ◽  
Dimensionless Numbers ◽  
Flow Rates ◽  
Contact Condensation

Direct Contact Condensation tests have been conducted by injecting a mixture of steam and nitrogen into a subcooled water pool in a stainless steel tank through a vertical nozzle. The condensation rate, related to the heat transfer rate in the liquid side, was obtained by the difference of the gas inlet flow rates and the mass accumulation due to the bubble growth. By the measurements of steam and nitrogen flow rates and visualization of the bubble size variation, the heat transfer parameters in the liquid domain during the bubble formation, are obtained. The Nusselt number has been correlated with the dimensionless combination of fluid flow, system state and thermal properties of fluids. A least square approach has been applied to determine the exponent coefficients of dimensionless numbers in the correlations. It was found that the Nusselt number can be correlated by a function of the Jakob number, gas Peclet number, noncondensable concentration, liquid and gas density ratio and Eotvos number based on the current database.

Experimental Study of Direct Contact Condensation in the Presence of Noncondensable Gas

2002 ◽  
Author(s):  
Yiban Xu ◽  
Shripad T. Revankar ◽  
Mamoru Ishii
Keyword(s):  
Bubble Size ◽  
Direct Contact ◽  
High Speed ◽  
Size Variation ◽  
Saturated Steam ◽  
Dimensionless Numbers ◽  
Noncondensable Gas ◽  
Digital Format ◽  
System Pressure ◽  
Contact Condensation

A series of direct contact condensation tests of mixture of saturated steam and nitrogen has been carried out in a subcooled pool of water. Nitrogen is used as the noncondensable gas. A mixture of nitrogen and steam is discharged into the subcooled water pool through a vertical nozzle. The apparatus is equipped with appropriate instruments and flow visualization. Pre-heaters and super-heaters are used to heat up nitrogen and steam before they are mixed. Tests have been preformed with variations of the liquid temperature, system pressure, nozzle size and the concentration of noncondensable gas. Images of bubble behaviors are captured with high speed video camera and downloaded into a PC in digital format. Information on bubble size variation and formation frequency is obtained from the image analysis. Detaching bubble size, surface area and frequency are correlated with the various dimensionless numbers.

Physical Interpretation of Flow and Heat Transfer in Preswirl Systems

2006 ◽  
Vol 129 (3) ◽  
pp. 769-777 ◽  
Author(s):  
Paul Lewis ◽  
Mike Wilson ◽  
Gary Lock ◽  
J. Michael Owen
Keyword(s):  
Heat Transfer ◽  
Reynolds Number ◽  
Nusselt Number ◽  
Turbulent Flow ◽  
Gas Turbines ◽  
Flow Parameter ◽  
Rotating Disk ◽  
Turbine Rotor ◽  
Scaled Model ◽  
Flow Rates

This paper compares heat transfer measurements from a preswirl rotor–stator experiment with three-dimensional (3D) steady-state results from a commercial computational fluid dynamics (CFD) code. The measured distribution of Nusselt number on the rotor surface was obtained from a scaled model of a gas turbine rotor–stator system, where the flow structure is representative of that found in an engine. Computations were carried out using a coupled multigrid Reynolds-averaged Navier-Stokes (RANS) solver with a high Reynolds number k-ε∕k-ω turbulence model. Previous work has identified three parameters governing heat transfer: rotational Reynolds number (Reϕ), preswirl ratio (βp), and the turbulent flow parameter (λT). For this study rotational Reynolds numbers are in the range 0.8×106<Reϕ<1.2×106. The turbulent flow parameter and preswirl ratios varied between 0.12<λT<0.38 and 0.5<βp<1.5, which are comparable to values that occur in industrial gas turbines. Two performance parameters have been calculated: the adiabatic effectiveness for the system, Θb,ad, and the discharge coefficient for the receiver holes, CD. The computations show that, although Θb,ad increases monotonically as βp increases, there is a critical value of βp at which CD is a maximum. At high coolant flow rates, computations have predicted peaks in heat transfer at the radius of the preswirl nozzles. These were discovered during earlier experiments and are associated with the impingement of the preswirl flow on the rotor disk. At lower flow rates, the heat transfer is controlled by boundary-layer effects. The Nusselt number on the rotating disk increases as either Reϕ or λT increases, and is axisymmetric except in the region of the receiver holes, where significant two-dimensional variations are observed. The computed velocity field is used to explain the heat transfer distributions observed in the experiments. The regions of peak heat transfer around the receiver holes are a consequence of the route taken by the flow. Two routes have been identified: “direct,” whereby flow forms a stream tube between the inlet and outlet; and “indirect,” whereby flow mixes with the rotating core of fluid.

An Analysis of a Direct Contact Ice Slurry Generator

2008 ◽  
Author(s):  
M. A. Wahed ◽  
M. N. A. Hawlader
Keyword(s):  
Heat Transfer ◽  
Simulation Model ◽  
Direct Contact ◽  
Coolant Flow ◽  
Temperature Profiles ◽  
Ice Slurry ◽  
Generation System ◽  
Contact Heat ◽  
Flow Rates ◽  
Contact Heat Transfer

Attempts have been made to study an ice slurry generation system where two immiscible liquids, water and a coolant, are used to produce ice slurry by direct contact heat transfer. A mathematical model has been developed to evaluate the heat transfer phenomena between the coolant drops and the water in the ice slurry generation system. In this process, all the important variables that affect the direct contact heat transfer between these two fluids were incorporated into the simulation model to evaluate thermal performance of the system. Experiments were performed on an ice slurry generator using water and an immiscible liquid coolant, Fluroinert FC-84. The coolant at about −10°C to −15°C was delivered to the top of the ice slurry generator containing water and collected from the bottom for recirculation. The measured temperature profiles of water in the ice slurry generator for different coolant flow rates (8 lit/min to 12 lit/min) showed a good agreement with those temperature profiles obtained from the simulation model. These results validated the simulation model developed for the ice slurry generator. The analysis showed that during sensible cooling, the estimated heat transfer coefficients between water and the coolant were in the range of 3.0 to 6.5 kW/m2 for coolant flow rates varying from 8 lit/min to 12 lit/min. Higher coolant flow rates also enhanced the ice formation process due to the increased heat transfer rate. In addition, it was also observed that the ice production increased significantly when the nozzle was placed at the bottom of the ice slurry generator.

Finite element analysis of water-based Ferrofluid flow in a partially heated triangular cavity

2020 ◽  
Vol ahead-of-print (ahead-of-print) ◽  
Author(s):  
Muhammad Usman ◽  
Muhammad Hamid ◽  
Zafar Hayat Khan ◽  
Rizwan Ul Haq ◽  
Waqar Ahmed Khan
Keyword(s):  
Heat Transfer ◽  
Finite Element ◽  
Nusselt Number ◽  
Volume Fraction ◽  
Vertical Wall ◽  
Heating Element ◽  
Dimensionless Temperature ◽  
Dimensionless Numbers ◽  
Element Analysis ◽  
Content Type

Purpose This study aims to deal with the numerical investigation of ferrofluid flow and heat transfer inside a right-angle triangular cavity in the presence of a magnetic field. The vertical wall is partially heated, whereas other walls are kept cold. The effects of thermal radiation are included in the analysis. The governing equations including continuity, momentum and energy equations are converted to nondimensional form using viable variables. Design/methodology/approach Finite element method (FEM)-based simulations are performed using finite element approach to investigate the effects of the volume fraction of ferroparticles (Fe3O4), the length of the heating element and the dimensionless numbers including Rayleigh and Hartmann numbers on the streamlines, isotherms and Nusselt number. Findings It is demonstrated that both horizontal and vertical velocity components increase with the length of the heating element, whereas the dimensionless temperature decreases the heating domain. It is observed that an increase of 10% in the volume fraction of ferroparticles increases Nusselt number more than 12%, and 20% increase in the volume fraction of ferroparticles increases more than 30%, depending upon the length of the heating element. Originality/value This is a new study showing the significance of the magnetic nanoparticles for the enhancement of heat transfer rate in a triangular cavity.

Influence of Fluid-Dynamics on Heat Transfer in a Pre-Swirl Rotating-Disc System

2004 ◽  
Author(s):  
Gary D. Lock ◽  
Michael Wilson ◽  
J. Michael Owen
Keyword(s):  
Heat Transfer ◽  
Nusselt Number ◽  
Gas Turbines ◽  
Fluid Dynamic ◽  
Impinging Jets ◽  
Coolant Flow ◽  
Viscous Effects ◽  
Rotating Disc ◽  
Scaled Model ◽  
Flow Rates

Modern gas turbines are cooled using air diverted from the compressor. In a “direct-transfer” pre-swirl system, this cooling air flows axially across the wheel-space from stationary pre-swirl nozzles to receiver holes located in the rotating turbine disc. The distribution of the local Nusselt number, Nu, on the rotating disc is governed by three non-dimensional fluid-dynamic parameters: pre-swirl ratio, βp, rotational Reynolds number, Reφ, and turbulent flow parameter, λT. This paper describes heat transfer measurements obtained from a scaled model of a gas turbine rotor-stator cavity, where the flow structure is representative of that found in the engine. The experiments reveal that Nu on the rotating disc is axisymmetric except in the region of the receiver holes, where significant two-dimensional variations have been measured. At the higher coolant flow rates studied, there is a peak in heat transfer at the radius of the pre-swirl nozzles, associated with the impinging jets from the pre-swirl nozzles. At lower coolant flow rates, the heat transfer is dominated by viscous effects. The Nusselt number is observed to increase as either Reφ or λT increases.

Heat transfer rate of direct-contact condensation on baffle trays

2008 ◽  
Vol 51 (25-26) ◽  
pp. 5772-5776 ◽  
Author(s):  
Srbislav B. Genić ◽  
Branislav M. Jaćimović ◽  
Ljubiša A. Vladić
Keyword(s):  
Heat Transfer ◽  
Heat Transfer Rate ◽  
Direct Contact ◽  
Transfer Rate ◽  
Contact Condensation

Physical Interpretation of Flow and Heat Transfer in Pre-Swirl Systems

2006 ◽  
Author(s):  
Paul Lewis ◽  
Mike Wilson ◽  
Gary Lock ◽  
J. Michael Owen
Keyword(s):  
Heat Transfer ◽  
Reynolds Number ◽  
Nusselt Number ◽  
Turbulent Flow ◽  
Gas Turbines ◽  
Flow Parameter ◽  
Swirl Flow ◽  
Rotating Disc ◽  
Scaled Model ◽  
Flow Rates

This paper compares heat transfer measurements from a pre-swirl rotor-stator experiment with 3D steady state results from a commercial CFD code. The measured distribution of Nusselt number on the rotor surface was obtained from a scaled model of a gas turbine rotor-stator system, where the flow structure is representative of that found in an engine. Computations were carried out using a coupled multigrid RANS solver with a high-Reynolds-number k-ε/k-ω turbulence model. Previous work has identified three parameters governing heat transfer: rotational Reynolds number (Reφ), pre-swirl ratio (βp) and the turbulent flow parameter (λT). For this study rotational Reynolds numbers are in the range 0.8×106 &lt; Reφ &lt; 1.2×106. The turbulent flow parameter and pre-swirl ratios varied between 0.12 &lt; λT &lt; 0.38 and 0.5 &lt; βp &lt; 1.5, which are comparable to values that occur in industrial gas turbines. At high coolant flow rates, computations have predicted peaks in heat transfer at the radius of the pre-swirl nozzles. These were discovered during earlier experiments and are associated with the impingement of the pre-swirl flow on the rotor disc. At lower flow rates, the heat transfer is controlled by boundary-layer effects. The Nusselt number on the rotating disc increases as either Reφ or λT increases, and is axisymmetric except in the region of the receiver holes, where significant two-dimensional variations are observed. The computed velocity field is used to explain the heat transfer distributions observed in the experiments. The regions of peak heat transfer around the receiver holes are a consequence of the route taken by the flow. Two routes have been identified: “direct”, whereby flow forms a stream-tube between the inlet and outlet; and “indirect”, whereby flow mixes with the rotating core of fluid. Two performance parameters have been calculated: the adiabatic effectiveness for the system, Θb,ab, and the discharge coefficient for the receiver holes, CD. The computations show that, although Θb,ab increases monotonically as βp increases, there is a critical value of βp at which CD is a maximum.

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