Track 1 TOC Proceedings Proceedings of HT2003 of 2003ASME ASMESummer Summer Heat Transfer Conference Heat Transfer Conference July 21–23, 2003, Las Vegas, Nevada, USA July 21-23, 2003, Las Vegas, Nevada, USA HT2003-47455 HT2003-47455 TRANSIENT RADIATIVE TRANSFER OF LIGHT PULSE PROPAGATION IN THREEDIMENSIONAL SCATTERING MEDIA WITH FINITE VOLUME METHOD AND INTEGRAL EQUATION MODEL Xiaodong Lu and Pei-feng Hsu Mechanical and Aerospace Engineering Department Florida Institute of Technology Melbourne, Florida 32901, U.S.A. and John C. Chai School of Mechanical and Production Engineering Nanyang Technological University Singapore 639798 INTRODUCTION The transient radiative transfer process is studied with a finite volume method (FVM) and an integral equation (IE) model. Propagation of a short light pulse in the three-dimensional absorbing and isotropic scattering media is considered. Collimated irradiation enters at one side of the rectangular medium. The other five boundaries are cold and black, nonparticipating surfaces. The spatial and temporal distributions of the integrated intensity and radiative flux are obtained. thick media. Furthermore, these methods can't resolve the wave front and miss important physical detailed information in the early stage of the transient process. It is therefore essential and critical to develop accurate solution models to advance the application of transient radiation transport, especially the use of ultra-short pulsed lasers for optical imaging and remote sensing. In this study, the results from two different solution methods are compared and the effect of scattering albedo on a base case is examined using the integral equation model. There are many existing models that have been used to treat transient radiation processes: from the earlier work of Monte Carlo method to more recently the discrete ordinates, finite volume, and integral equation methods. Most existing transient models either failed to address the hyperbolic wave nature of the process or relied on the approximations that simplify the transport equation, e.g., diffusion approximation and spherical harmonics approximation, and the geometry under consideration was usually a one-dimensional slab except a few cases, where two- and three-dimensional rectangular geometries were studied. An evident drawback of the these solution methods is the failure to predict the correct propagation speed within the medium as well as inadequate solution accuracy except under certain conditions like optically NOMENCLATURES a coefficient of the FVM discretization equation b source term of the FVM discretization equation c propagation speed of radiation transport in the medium l l Dcw , Dce direction cosine integrated over ∆Ω l l l Dcs , Dcn direction cosine integrated over ∆Ω l l l Dcb , Dct direction cosine integrated over ∆Ω l G incident radiation, integrated intensity, or fluence rate I radiation intensity 1 Copyright©©2003 2003by byASME ASME Copyright kˆ unit vector in the z-direction radiative flux geometric path length sˆ unit vector along a given direction t time u unit step function x, y, z rectangular coordinates M total number of control angles ± ± S cb , S pb additional source terms for high-resolution scheme ± S± S ce , pe additional source terms for high-resolution scheme ± S± S cn , pn additional source terms for high-resolution scheme ± ± S cs , S ps additional source terms for high-resolution scheme S ct± , S ±pt additional source terms for high-resolution scheme ± S cw , S ±pw additional source terms for high-resolution scheme l Sm modified source function q s TRANSIENT RADIATION TRANSPORT PROCESS The transient radiative transfer equation (TRTE) in an absorbing, non-emitting, and scattering medium in direction sˆ can be written as (Ozisik, 1973) ∂I (x, y , z , sˆ, t ) ∂I (x, y , z , sˆ, t ) + = − β I (x, y , z , sˆ, t ) c∂t ∂s + σ I (x, y , z , sˆ ′, t ) Φ(sˆ ′, sˆ ) dΩ ∫ 4π Ω =4π (1) FINITE-VOLUME METHOD The TRTE for a discrete direction l can be written as ∂I l ∂I l l + = − β ml I l + S m ∂s c∂t (2) where the modified extinction coefficient β ml and the modified l source function S m are (Chai et al., 1994) Greek symbols β extinction coefficient κ absorption coefficient σ scattering coefficient τ optical thickness of the medium, β zo θ polar angle ϕ azimuthal or circumferential angle Φ scattering phase function Ω solid angle ω scattering albedo β ml = κ + σ − l = κI b + Sm σ 4π σ Φ ll ∆Ω l (3a) l ′ l ′l l′ ∑ I Φ ∆Ω (3b) 4π M l ′=1,l ′≠l Following the procedure outlined in Chai (2003), the final discretization equation for a typical three-dimensional control volume (Fig. 1a) and control angle (Fig. 1b) can be written as l l a Pl I Pl = aW IW + a El I El + a Sl I Sl Subscripts B blackbody C collimated component or direction E, W, N, S, B, T east, west neighbors of P e, w,n, s,b, t east, west control-volume faces WW west neighbor of W P control volume p pulse temporal width v quantity related to the volume element w quantity related to the surface (or wall) element l + a lN I N + a Bl I Bl + aTl I Tl + b l (4a) where l a El = − Ae Dce l l aW = − Aw D cw (4b) l a lN = − An Dcn l a Sl = − As Dcs (4c) l aTl = − At Dct l a Bl = − Ab Dcb (4d) l l l a Pl = Ae Dce + Aw Dcw + An Dcn l l l + As Dcs + Ab Dcb + At Dct Superscripts ' dummy variables ^ vector o previous time step l angular directions + β ml , p ∆V P ∆Ω l + l l bl = Sm ,P ∆V P ∆Ω + 2 (4e) ∆v∆Ω l + S c,CLAM c ∆v∆Ω l o I P + S p ,CLAM c (4f) Copyright©©2003 2003by byASME ASME Copyright perpendicular to the z = 0 wall. participating radioactively. In Eq. (4), SCCLAM and Sp,CLAM are the extra source terms due to the CLAM scheme. The time evolution of the incident radiation at five spatial locations namely, z/L = 1/34, 9/34, 1/2, 25/34, and 33/34 are plotted in Fig. 2. Results obtained using the IE and FV methods are shown. The step and CLAM schemes are used with the FV method. Overall, the IE method is more accurate than the FV method. Due to false scattering, the FV method solutions spread over a larger time interval as time increases. As expected, the step scheme produces more spreading than the CLAM scheme. This leads to lower peak incident intensities at the various spatial locations. At a given location, it is also noticed that radiation penetrates much faster and attenuates much slower with the step scheme. The solutions obtained using the CLAM scheme are slightly better than those of the step scheme. However, it also predicted lower peak incident radiation, faster penetration time and slower decay time than the IE formulation. INTEGRAL EQUATION MODEL Following the procedure described in Tan and Hsu (2001; 2002), the integrated intensity is G ( x, y , z , t ) = ∫4π I (x w , y w ,0, sˆ, t − s / c )e − βs dΩ [ ] 1 s − β ( s − s ′) ′ ds dΩ ∫ ∫ σ ( x ′, y ′, z ′)G (x ′, y ′, z ′, t 2′ )e 4π 4π 0 I (x w , y w ,0, sˆ, t − s / c )e − βs = ∫∫A(t ) cosθdA (5) s2 + + 1 σ (x ′, y ′, z ′)G ( x ′, y ′, z ′, t ′)e − β ( s − s ) dV ∫∫∫V (t ) 4π ( s − s ′) 2 ′ The boundary condition is a cube with one black and diffusely emitting surface at z = 0 and the other five surfaces are cold and black (or transparent). For a collimated pulse with the intensity I0 is suddenly emitted from boundary at z = 0 at the instant of t = 0 and turned off at t = tp, then it can be expressed as [ ( )] I (x w , y w ,0, sˆ, t ) = I 0 u (t ) − u t − t p kˆ An improvement of the FVM result can readily be made is by decomposing the intensity into the collimated and diffuse components (Sakami, et al. 2000), I ( x, y, z , sˆ, t ) = I c ( x, y, z , sˆc , t ) + I d ( x, y, z , sˆ, t ) (6) z z z 1 G (x, y, z , t ) = I 0 u t − − u t − − t p e −κz + u t − ⋅ 4π c c c ∫∫∫ − β ( x − xv )2 +( y − yv )2 +( z − z ′)2 ( x − x v ) 2 + ( y − y v ) 2 + ( z − z ′) 2 (8) In this equation, Ic is the residual intensity of the collimated beam after extinction, and Id is the diffuse intensity, which is the result of the scattered radiation away from the collimated beam. where k̂ is the unit vector along the collimated beam direction, i.e., z-axis. The resulting equation of G is σ (x ′, y ′, z ′)G ( x ′, y ′, z ′, t ′)e The other walls are not dx v dy v dz ′ (7) Equation (7) is a Volterra integral equation of the second kind. The numerical quadrature used in solving this equation is based on the YIX method (Hsu, et al. 1993). An asymmetric spherical ring angular quadrature set is used in the spatial integration (Lu and Hsu, 2003). The integration limit is a time dependent domain of influence, which is detailed in Tan and Hsu (2002) and will not be repeated here. RESULTS AND DISCUSSION In this article, transient radiative transfer in a cube subjected to a collimated beam is examined. The cold medium absorbs and scatters energy isotropically. The optical thickness of the medium is 1. Three scattering albedoes namely, 0.1, 0.5 and 1 are examined. The collimated beam enters the domain 3 The effect of scattering albedo is shown in figures 3-5. In Fig. 3, there are several crossovers of the temporal curves at different locations. This is caused by the drastic change in the slope of the temporal curves. For example, the G function has a sudden drop in magnitude near t/∆t = 35. This corresponds to the temporal variation in the domain of influence, i.e., abrupt change in the volume integration limit of Eq. (7). Similar temporal changes are also observed at other locations. In fact, the crossover occurs several times over the duration of the simulation. Same crossover is also seen in the other two cases (Figs. 4 and 5). However, the effect becomes weaker as albedo increases. This is expected as the volume integration term, the second term on the right hand side of Eq. (7), become more important as albedo increases. The higher signal level in large albedo case tends to smear out the crossover. In all cases, the multiple, diffuse scattering effect is not very significant because the optical thickness is relatively small. For a typical pulse laser probed medium, optical thickness in the order of 100 and albedo close to 1 is very common (Hsu, 2000). In that case, stronger diffuse scattering will result a second, stronger signal level peak observed in the experiments and our earlier numerical work. 3 Copyright 2003 ASME Copyright ©© 2003 byby ASME CONCLUSION Among several transient radiation transport processes, we believe the collimated pulse irradiation problem presents a good test of the numerical models as well as close relevance to actual physical applications. A high order upwind scheme that can capture and resolve wave front is essential. This study compares two important methods: finite volume method and integral equation model. The CLAM scheme is more accurate than the simple step scheme used in finite volume method. However, both schemes are unable to recover the correct propagation speed as is the integral equation model. The effect of scattering is not very significant in the case of unity optical thickness of the medium. The effect will be more significant in larger optical thickness media. Future work will include the temporal reflectance and transmittance signals of pulse irradiated nonhomogeneous media. Hsu, P.-f. (2001), "Effects of Multiple Scattering and Reflective Boundary on the Transient Radiative Transfer Process," Int. J. of Thermal Sciences, Vol. 40, No. 6, pp. 539-549. Hsu, P.-f., Z. Tan and J. R. Howell (1993), "Radiative Transfer by the YIX Method in Nonhomogeneous, Scattering and Non-Gray Medium," AIAA J. Thermophysics and Heat Transfer Vol. 7, No. 3, pp.487-495. Lu, X. and P.-f. Hsu (2003), "Parallel Computing Performance of Two Numerical Quadratures for an Integral Formulation of Transient Radiative Transfer Process," under review in AIAA J. Thermophysics and Heat Transfer. Ozisik, M. N. (1973), Radiative Transfer and Interaction with Conduction and Convection, J. Wiley, New York. Sakami, M., K. Mitra, and P.-f. Hsu (2000), "Transient Radiative Transfer in Anisotropically Scattering Media using Monotonicity-Preserving Schemes," ASME 2000 Int. Mechanical Engineering Congress & Exposition, ASME HTD-Vol. 366-1, pp. 135-143, Orlando, FL, November 2000. Tan, Z.-M., and P.-f. Hsu (2001), "An Integral Formulation of Transient Radiative Transfer," ASME J. Heat Transfer, Vol. 123, No. 3, pp.466-475. Tan, Z.-M., and P.-f. Hsu (2002), "Transient Radiative Transfer in Three-Dimensional Homogeneous and Nonhomogeneous Participating Media," J. Quant. Spect. & Rad. Transfer, Vol. 73, No. 2-5, pp. 181-194. References Chai, J. C. (2003), "One-Dimensional Transient Radiation Heat Transfer Modeling Using a Finite-Volume Method," Numerical Heat Transfer, Part B, Accepted for publication. Chai, J. C., H. S. Lee, and S. V. Patankar, (1994), "Improved Treatment of Scattering Using the Discrete Ordinates Method," ASME J. Heat Transfer, Vol. 116, No. 1, pp. 260263. 4 Copyright©©2003 2003by byASME ASME Copyright N 10 T n t P E e W B G(0,0,z,t) w s b 0 10 -1 10 -2 10 -3 10 -4 10 -5 10 -6 z 0 20 G(0,0,z,t) y + φ− φ x 40 50 10 -1 10 -2 10 -3 10 -4 10 -5 10 -6 IE CLAM Step 1/2 0.6 G(0,0,z,t) 9/34 25/34 33/34 0.4 0.2 10 t/∆t 15 ω = 0.5 0 10 1 z/L=1/34 z=1/34 z=9/34 z=1/2 z=25/34 z=33/34 10 20 t/∆t 30 40 50 Figure 4: Pulse propagation in three-dimensional media with scattering albedo = 0.5, based on IE model. Figure 1: (a) A typical two-dimensional control volume, (b) a typical control angle. 5 30 0 (b) 0.8 t/∆t Control angle, ∆Ωl θ− θ+ G(0,0,z,t) 10 Figure 3: Pulse propagation in three-dimensional media with scattering albedo = 0.1, based on IE model. 10 0 ω = 0.1 S (a) 0 z=1/34 z=9/34 z=1/2 z=25/34 z=33/34 20 0 10 -1 10 -2 10 -3 10 -4 10 -5 10 -6 z=1/34 z=9/34 z=1/2 z=25/34 z=33/34 ω=1 0 10 20 t/∆t 30 40 50 Figure 5: Pulse propagation in three-dimensional media with scattering albedo = 1, based on IE model. Figure 2: Comparison of integral equation model and finite volume method with two difference schemes (CLAM and step). 5 Copyright©©2003 2003by byASME ASME Copyright
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