Study Group Report: Plate-fin Heat Exchangers: AEA Technology

Similar documents
EXPERIMENTAL STUDY ON DISCHARGE COEFFICIENT OF OUTFLOW OPENING FOR PREDICTING CROSS-VENTILATION FLOW RATE

Electric Current and Resistance

Module 4: General Formulation of Electric Circuit Theory

Short notes for Heat transfer

Compressibility Effects

Chapter 11: Atmosphere

Chapter 4. Unsteady State Conduction

bulk velocity through orifice,

CS 477/677 Analysis of Algorithms Fall 2007 Dr. George Bebis Course Project Due Date: 11/29/2007

, which yields. where z1. and z2

7.0 Heat Transfer in an External Laminar Boundary Layer

1/2 and e0 e s ' 1+ imm w 4 M s 3 πρ0 r 3 m. n 0 ktr. .Also,since n 0 ktr 1,wehave. 4 3 M sπρ 0 r 3. ktr. 3 M sπρ 0

General Chemistry II, Unit I: Study Guide (part I)

Guide to Using the Rubric to Score the Klf4 PREBUILD Model for Science Olympiad National Competitions

Use a lens holder fabricated from SiC. SiC has a larger CTE than C-C, i.e. it is better matched to the SFL6.

February 28, 2013 COMMENTS ON DIFFUSION, DIFFUSIVITY AND DERIVATION OF HYPERBOLIC EQUATIONS DESCRIBING THE DIFFUSION PHENOMENA

Math Foundations 20 Work Plan

Pressure And Entropy Variations Across The Weak Shock Wave Due To Viscosity Effects

Lecture 17: Free Energy of Multi-phase Solutions at Equilibrium

Thermodynamics and Equilibrium

Lab 1 The Scientific Method

NAME TEMPERATURE AND HUMIDITY. I. Introduction

NGSS High School Physics Domain Model

Sections 15.1 to 15.12, 16.1 and 16.2 of the textbook (Robbins-Miller) cover the materials required for this topic.

Phys101 Final Code: 1 Term: 132 Wednesday, May 21, 2014 Page: 1

Introductory Thoughts

arxiv:hep-ph/ v1 2 Jun 1995

MANIPAL INSTITUTE OF TECHNOLOGY

Differentiation Applications 1: Related Rates

BASIC DIRECT-CURRENT MEASUREMENTS

FIELD QUALITY IN ACCELERATOR MAGNETS

and the Doppler frequency rate f R , can be related to the coefficients of this polynomial. The relationships are:

Solution to HW14 Fall-2002

ECE 5318/6352 Antenna Engineering. Spring 2006 Dr. Stuart Long. Chapter 6. Part 7 Schelkunoff s Polynomial

Examiner: Dr. Mohamed Elsharnoby Time: 180 min. Attempt all the following questions Solve the following five questions, and assume any missing data

Computational modeling techniques

I understand the new topics for this unit if I can do the practice questions in the textbook/handouts

Fall 2013 Physics 172 Recitation 3 Momentum and Springs

LHS Mathematics Department Honors Pre-Calculus Final Exam 2002 Answers

( ) kt. Solution. From kinetic theory (visualized in Figure 1Q9-1), 1 2 rms = 2. = 1368 m/s

Chapter 39. A GUIDE TO THE DESIGN OP AIR BUBBLERS FOR MELTING ICE Simon Ince Hydraulics Section, National Research Council Ottawa, Canada

More Tutorial at

READING STATECHART DIAGRAMS

Physics 2B Chapter 23 Notes - Faraday s Law & Inductors Spring 2018

Physics 262/266. George Mason University. Prof. Paul So

(1.1) V which contains charges. If a charge density ρ, is defined as the limit of the ratio of the charge contained. 0, and if a force density f

Department of Economics, University of California, Davis Ecn 200C Micro Theory Professor Giacomo Bonanno. Insurance Markets

Process Engineering Thermodynamics E (4 sp) Exam

Least Squares Optimal Filtering with Multirate Observations

Modelling of Clock Behaviour. Don Percival. Applied Physics Laboratory University of Washington Seattle, Washington, USA

I. Analytical Potential and Field of a Uniform Rod. V E d. The definition of electric potential difference is

Charge of an Electron

A New Evaluation Measure. J. Joiner and L. Werner. The problems of evaluation and the needed criteria of evaluation

Chapters 29 and 35 Thermochemistry and Chemical Thermodynamics

Chem 115 POGIL Worksheet - Week 12 Molecular Shapes

How do scientists measure trees? What is DBH?

THERMAL-VACUUM VERSUS THERMAL- ATMOSPHERIC TESTS OF ELECTRONIC ASSEMBLIES

Feasibility Testing Report Muscle Optimization Stage I

Lecture 02 CSE 40547/60547 Computing at the Nanoscale

Relationships Between Frequency, Capacitance, Inductance and Reactance.

CHAPTER 13 Temperature and Kinetic Theory. Units

Chapter 16. Capacitance. Capacitance, cont. Parallel-Plate Capacitor, Example 1/20/2011. Electric Energy and Capacitance

Introduction to Spacetime Geometry

22.54 Neutron Interactions and Applications (Spring 2004) Chapter 11 (3/11/04) Neutron Diffusion

Science 9 Unit 2: Atoms, Elements and Compounds

Phys. 344 Ch 7 Lecture 8 Fri., April. 10 th,

Thermodynamics Partial Outline of Topics

Aircraft Performance - Drag

Displacement and Deflection Sensitivity of Gas-coupled Laser Acoustic. Detector

Math Foundations 10 Work Plan

Lead/Lag Compensator Frequency Domain Properties and Design Methods

Figure 1a. A planar mechanism.

Physics 2010 Motion with Constant Acceleration Experiment 1

General Chemistry II, Unit II: Study Guide (part 1)

3. Design of Channels General Definition of some terms CHAPTER THREE

Advanced Heat and Mass Transfer by Amir Faghri, Yuwen Zhang, and John R. Howell

Kepler's Laws of Planetary Motion

7 TH GRADE MATH STANDARDS

Assume that the water in the nozzle is accelerated at a rate such that the frictional effect can be neglected.

Chemistry 20 Lesson 11 Electronegativity, Polarity and Shapes

Charge of an Electron

Measurement of Radial Loss and Lifetime. of Microwave Plasma in the Octupo1e. J. C. Sprott PLP 165. Plasma Studies. University of Wisconsin DEC 1967

COASTAL ENGINEERING Chapter 2

Determining the Accuracy of Modal Parameter Estimation Methods

A PLETHORA OF MULTI-PULSED SOLUTIONS FOR A BOUSSINESQ SYSTEM. Department of Mathematics, Penn State University University Park, PA16802, USA.

PSU GISPOPSCI June 2011 Ordinary Least Squares & Spatial Linear Regression in GeoDa

Revision: August 19, E Main Suite D Pullman, WA (509) Voice and Fax

Building to Transformations on Coordinate Axis Grade 5: Geometry Graph points on the coordinate plane to solve real-world and mathematical problems.

Matter Content from State Frameworks and Other State Documents

Name: Period: Date: BONDING NOTES ADVANCED CHEMISTRY

ChE 471: LECTURE 4 Fall 2003

GAUSS' LAW E. A. surface

Information for Physics 1201 Midterm I Wednesday, February 20

Beam Expander Basics: Not All Spots Are Created Equal

3. Mass Transfer with Chemical Reaction

ENSC Discrete Time Systems. Project Outline. Semester

Derailment Safety Evaluation by Analytic Equations

The Journal of Supercritical Fluids

ANALYTICAL SOLUTIONS TO THE PROBLEM OF EDDY CURRENT PROBES

ALE 21. Gibbs Free Energy. At what temperature does the spontaneity of a reaction change?

Transcription:

Study Grup Reprt: Plate-fin Heat Exchangers: AEA Technlgy The prblem under study cncerned the apparent discrepancy between a series f experiments using a plate fin heat exchanger and the classical thery f Nusselt. A plate fin heat exchanger invlves the flw f a stream f cndensing nitrgen vapur in ne flw channel and a cunterflwing stream f liquid nitrgen in an adjacent flw channel. The liquid nitrgen is at a lwer temperature and pressure and bils. The classical thery f Nusselt treats the flw f the cndensing vapur using lubricatin thery. A liquid film f cndensate frms n the walls f the flw channel, and drains under gravity. As the flw cntinues alng the channel, further cndensatin ccurs and the flux f liquid increases (figure 1). Simple lubricatin thery analysis suggests that the mass flux f the liquid per unit width n a flat plate is This may be used t determine the quality, Q, which i~ a measure f the vapur flux divided by the ttal flux. where M is the ttal mass flux. Nte the quality may alternatively be defined as a thermdynamic quality, in which case the rati f the enthalpy (rather than mass) fluxes is used in the definitin, with the liquid and vapur enthalpies being evaluated at the cndensatin temperature. The relatinship between the quality and the mass flux f liquid enables ne t determine the heat transfer cefficient as a functin f the quality. The heat transfer thrugh the liquid film n the walls has the frm, apprximately, where T; is the cndensatin temperature f the vapur and Tw is the wall temperature, and K is the thermal cnductivity. The film thickness h may be recast in terms f the quality, using the abve analysis, t yield the result This simple thery was applied t understand the variatin f the heat transfer cefficient with quality alng ne f the rectangular plate fin passages in a test heat exchanger at 1

Harwell. The thery was adapted t include the effects f the gemetry f the rectangular cavity and the reduced efficiency f the secndary fins, which are nt directly in cntact with the cunterflwing channel. Hwever, in spite f these crrectins t the simple thery, the variatin f the experimental heat transfer cefficients with quality differed frm the scaling suggested abve (figure 2). At high flw rates the dimensinless heat transfer cefficient varied smewhat mre slwly than predicted by the Nusselt scaling, while at lw flw rates the heat transfer cefficient decreased mre rapidly than predicted by the Nusselt thery. The scaling parameter, which includes the effect f the gemetry may be fund frm the data at imtermediate flw rates (figure 2). At the study grup, varius explanatins as t the surce f the discrepancy between the Nusselt thery and the data were explred. Tw appraches taken were t assess the data cllectin methd and t assess the relevance f the mdel t the experiments. Experimental assessment. The quality is calculated by measuring the heat flux thrugh the walls f the channel and then assuming that this heat flux is supplied by the latent heat released n cndensatin f the vapur. Therefre, at any distance dwn the pipe, the ttal flux f cndensed vapur may be estimated. Hwever, in analysing the data cllectin methds, it was fund that there is sme superheating f the nitrgen vapur n entry t the channel. This superheat remains in the vapur fr sme time, and affects the estimate f the pint at which cndensatin ccurs since the superheat is cnducted thrugh the wall in additin t the latent heat. In turn this affects the estimate f the quality. Hwever, frm the enthalpy balance, this superheating nly amunts t a quality errr f a few percent. Further, it was fund that the heat flux in the wall was nt in fact cnstant but varied significantly near the entry pint. The heat flux measurements in the wall were quite far apart, and did nt seem sufficient t reslve this variatin and thereby accurately estimate the ttal heat flux thrugh a given length f the wall. Indeed in sme experiments, nly ne r tw thermcuples were lcated in this entry regin. One cnclusin f the study grup is that the accuracy f these estimates culd be checked. Theretical Assessment. In additin, during the study grup week, we examined the assumptins implicit in the Nusselt thery, and their relevance t the flw in questin. A majr issue which was addressed was the rle f any indentatins in the walls, as arise fr example near sites f brazing between adjacent channel walls. In such narrw grves, the actin f surface tensin is t fill the grve with fluid, and thereby pssibly create a flw path f lwer resistance than n the smther walls f the flw channel. This can increase the flux f 2

liquid dwn the channel, but its efect upn the relatinship between the heat transfer cefficient (HTC) and the quality was nt clear. In rder t elucidate the pssible impact f any grves upn the HTC-quality relatinship, we develped a simple mdel f a grve f size d embedded in a plane wall, and aligned with the flw. A simple scaling f the lateral surface tensin frces and the dwnward gravitatinal frce, suggests that the frce rati is and s any grve f size smaller than Irnm will draw in fluid n a shrt timescale cmpared t the dwnward flw timescale. Furthermre, the lateral flux f cndensed liquid required t fill the grve may be supplied by the enhanced cndensatin arund the grve which results frm the thinning f the film arund the grve under the actin f surface tensin (figure 3). The effect f such a grve upn the Nusselt heat transfer thery is readily calculated, and shwn t be imprtant. The reasn that a flw in a grve changes the scaling is that the liquid flux may be significantly enhanced by such a grve whereas the heat flux thrugh the wall des nt change significantly. The liquid flux is given by the sum. f the lubricatin flw dwn the wall, f lateral scale a say, plus the flw in the grve itself, giving the ttal liquid flux ver a length a (figure 3) A simple scaling analysis shws that fr a grve f width 0.1 mm, a typical film thickness f 0.05 mm, and a channel width a f 1 mm, the flux rati between the flw in the grve and that in the main film is and s the flux is increased by O(1) wing t the presence f the grve. We can then write dwn the relatin In cntrast, the heat transfer thrugh the liquid film "Cnsistsf the sum f the flux thrugh the main film and that thrugh the grve. This has the apprximate value fr the gemetry f figure 3 a d Heatflux = kt:::.t(-;;, + (h+d)) 3

Nw the rati f the heat flux thrugh the grve and thrugh the film prper is dh (d+h)a"'o,l and s the heat flux is nt significantly altered by the presence f the liquid filled grve. As a result, the heat flux has the apprximate value K6Ta Heatflux = h and the heat transfer cefficient scales as t(l + O( (d!~)a». Using the revised frmula fr the liquid flux, we see that the heat transfer cefficient is related t the quality by the scaling The term n the right hand side is f sme imprt, as shwn abve, and crrespnds t the enhancement f the liquid flux wing t the presence f the grves. In figure 4, we shw hw this factr differs frm the classical Nusselt thery in which the scaling is simply (1 - Q)-1/3. Nte that the effect this crrectin is greatest at lw flw rates fr which the liquid in the film cnstitutes Experimental Design. a large fractin f the ttal flux. A further feature was nted abut the present experimental cnfiguratin. This sheds sme light upn the sensitivity f the apparatus cefficient with fin blade shape. design, mst f the temperature t detect changes in the heat transfer It was identified that with the present experimental drp between the cndensing vapur and the biling liquid in adjacent flw channels actually ccurs in the metal dividing the tw flw channels rather than in the liquid film f cndensate n the wall f the channel. In particular, if we balance the flux f heat thrugh the wall with that thrugh the liquid film, then T.' Tc - TWT.' T w - n..1'../ h =.l'-a h w where hw is the thickness f the wall and Tb is the biling temperature n the far side f the wall. Since the wall thickness in the experimental set-up is apprximately 6 mm, and the typical film thickness is 0.1 mm, then the temperature drp acrss the wall is abut 10 times larger than that acrss the film f cndensed vapur. As a result, the heat flux 4

acrss the walls f the channel is insensitive t small changes in the mean thickness f the liquid film as the gemetry f the channel is varied fr example, since the heat flux is determined by the temperature drp acrss the wall. Fr a given psitin ~ng the flw channel, in each experiment a cmparable mass f liquid will cndense in rder t supply the heat flu."{thrugh the wall. As a result, the quality at a given lcatin alng the wall will be relatively insensitive t differences in the detailed channel gemetry, and it is difficult t accurately cmpare the efficiency f different channel designs. In the real systems, the wall thickness is much smaller, and the heat flux is therefre mre sensitive t changes in the thickness f the liquid film, since mre f the temperature difference between the biling and cndensing flws ccurs acrss the cndensed liquid film. A different apprach might be t examine the prperties f the flw at varius pints alng the flw channel, by arranging a series f different length flw channels in series, and sampling the utput frm each channel. A number f questins emerge frm this reprt, including: (i) is there a critical heat flux? (ii) what size/shape f grve is best? (iii ) can mdels be tested using the existing experimental data? 5

~<---- Q. ----~) \ / kur.f!;,w- \ " "/~ 1~ (asj~it, <, " NuJJ-di ~) " ".......... " Q

~:L.z-> ~ ~ ~..... c Q) u '+- '"- Q) u L- Q) '+- Vl C U L- -+- - c 2-0 Vl ~ (1-3 J::. I.- (J I- \:s 2.. T Nusselt------- ---- -:::0-1 K uncertainty estimate in raw 6.T e e~/-vg McNaught (1987) / ~c = (1 7 I) 6. n = 0-22 In t::ql-gtin t. I... '::l n-.c -..- Vg,gas velcity + >2-0 increasing rj1<vg<2 ~ <1-0- (m/s~ PLAII'J FI N NITROGEN ALL DATA: 2-6 bar, 17-90 kg I m 2 s high shear regin where ( d P ) > 1-2 x 1. (d P ) dz T g dz TV ~-'- _ ;1;s~4i~~) ---------....... ------- 0-1 1 I I I I I I I 50 100 200 500 1000 2000- " I I I I L.J ~_--' I I ~ film Reynlds number f1~r-...j