Apparent Emissivity in the Base of a Cone Cosmin DAN, Gilbert DE MEY University of Ghent Belgium Overview 1. 2. 3. 4. 5. 6. 7. Introduction Description of the problem Configuration factors computation Apparent emissivity computation Genetic algorithms (GA) Results Conclusions Introduction • - Why to calculate the apparent emissivity? Build a black-body What kind of shapes has usually a black body Find the optimal shape Solve the radiative energy balance equations Write a computer program for apparent emissivity computation - Use a genetic algorithm optimization method Description of the problem • Circular cavities – Diffuse-gray surfaces – Known distribution of the temperature – Only radiative heat transfer – Known inner walls emissivity not depending on temperature – Known geometrical dimensions – Unknown apparent emissivity Description of the problem εapp εapp εapp εapp Description of the problem • The boundary integral equation q( r ) 1 ( r ) cos cos 4 4 T ( r ) [T ( r ) q( r )] dS 2 S (r ) ( r ) r r q(r ) q(r ) r r | r r | Description of the problem • The net radiation method ij 1 j Fi j q j j 1 j j N R N T j4 ( ij j 1 1 ij 0 Fi j ) N 4 4 F ( T T i j i j ) j 1 when i j when i j j i z Description of the problem • The net radiation method Aij qi Ci for i j aij for i j 1 (1 εi ) Fi j εi (1 ε j ) Fi j εj and – Gauss elimination method N ci εi (Ti T j4 Fi j ) 4 j 1 Configuration factors computation A2 r2 h r1 F12 1 2 R2 2 2 X X 4 ( ) R1 A1 X 1 1 R22 R12 r1 r2 with R1 and R2 h h Configuration factors computation Aj R Ai x Ai1 Ai2 Aj1 Aj2 1 Fi j A j1 ( F j1i 2 F j1i1 ) A j 2 ( F j 2i 2 F j 2i1 ) Ai Apparent emissivity – Radiative heat flux leaving the cavity – Radiative heat flux that would leave the cavity if it were a blackbody – Computation of the total heat flux for different particular cases with specified temperature – Find the highest value for apparent emissivity • Same length • Same open area • Different shapes for cavity Genetic algorithms – System for function optimisation – Adaptive search – iterative procedures – Variables = structures xi, population – Vector of parameters to the objective function f ( p1 , p2 ,... pn ) p1 1000 x1 (t ) p1 p2 ... pn 100011001110 P(t ) x1 (t ), x2 (t ),... x N (t ) Genetic algorithms Initialize population P(t) Evaluate objective function Complete terminate criteria No Select the best members Mate and mutate Replace old members Yes Printout results Genetic algorithms • Two steps to create a new population – Selection of the best members for replication – Alteration of the selected members using genetic operators: • Crossover – Two parents → two offspring's – 100011001111 and 011100110011 → 100011000011 and 011100111111 • Mutation – Alteration of one ore more bites in parent structure – 100011001111 → 100010001111 Genetic algorithms Genetic Algorithm Generate initial population Software Calculate the objective function (εapp) Generate the new population according with performances Check the terminate criteria Return results Return the value of the objective function for each structure Genetic algorithms R ’ ’ ’ P1 (z1 ,R1 ) P2(z2,R2) P1(z1,R1) P0(z0,R0) P3(z3,R3) •Termination criteria: Acceptable approximate solution Fixed total number of evaluations z Results 7.00E-10 Summation -relative error (%) 6.00E-10 5.00E-10 4.00E-10 3.00E-10 2.00E-10 1.00E-10 0.00E+00 1 51 101 151 201 Number of the surface (-) N Fij 1 j 1 where i 1...N 251 301 Results • Configuration factors from each surface to the open area: – Disk-to-disk method – Monte Carlo integration method • Configuration factors from each surface to all the others surfaces – Formula for differential configuration factors between two ring elements – The approximated formula e-2z Results 0.6 0.8 0.5 0.6 Fij cone angle 60° 0.4 0.3 0.4 cone angle 15° 0.2 0.2 0.1 0 0.00 0 0.20 0.40 z/L 0.60 0.80 1.00 Results Configuration factors [-] 0.025 0.02 differential formula exponential aproximation disk-to-disk 0.015 0.01 0.005 0 0 0.5 1 1.5 2 2.5 Cylinder length [m] 3 3.5 4 Results Relative difference [%] 6.00E-05 disk-to-disk and differential formula 5.00E-05 4.00E-05 3.00E-05 2.00E-05 1.00E-05 0.00E+00 0 0.5 1 1.5 2 2.5 Cylinder length [m] 3 3.5 4 Results Configuration factors [-] 0.03 disk-to-disk middle area disk-to-disk last area disk-to-disk first area 0.02 0.02 0.01 0.01 0.00 0 0.2 0.4 0.6 Cylinder length [-] 0.8 1 Results 60 q[W/m^2] cone 40 cylinder cone-cylinder 20 0 0 0.2 0.4 z/L 0.6 0.8 1 Absolute difference [W/m^2] Results 7 6 5 4 cylinder and conecylinder 3 cylinder and cone 2 1 0 0 0.2 0.4 z/L 0.6 0.8 1 Results 1 Apparent emissivity εwall=0.75 εwall=0.50 0.8 εwall=0.25 0.6 cone cylinder 0.4 0.2 0 2 4 6 8 10 L/R 12 14 16 18 20 Results Apparent emissivity 0.975 0.970 0.965 0.960 0.955 0.950 0.945 0 500 1000 Trials number 1500 Results R R ’ P1 (z1’,R1’) P2(z2,R2) P1(z1,R1) P0(z0,R0) • • • • • • P3(z3,R3) L=z3=30 cm; 0 ≤ z1 ≤ L; εwall=0.9 R1=R2=15 cm εapp=0.971 for z1=0.91 cm R1=R2=5 cm εapp=0.975 for z1=0.01 cm z P0(z0,R0) • • • • P1’(z1’,R1’) P2(z2,R2) P3(z3,R3) P1(z1,R1) z P4(z4,R4) L=z2=z3=z4=30 cm; 0 ≤ z1 ≤ L; εwall=0.9 R1=R2=10 cm; R3=2.5 cm εapp=0.9986 for z1=0.01 cm Conclusions • New tool for determination of the maximum value of the apparent emissivity • Results for configuration factors were verified and compared • Good agreement between the results • A software was written for the computation of the apparent emissivity • The software was combined with an optimisation genetic algorithm routine • The cylindrical cavities have higher apparent emissivities than the conical cavities for the same length and the same open area
© Copyright 2026 Paperzz