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Electron–Photon Shower Distribution Function. Tables for Lead, Copper and Air Absorbers PDF

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ELECTRON-PHOTON SHOWER DISTRIBUTION FUNCTION Tables for Lead, Copper and Air Absorbers BY H. MESSEL and D. F. CRAWFORD Φ PERGAMON PRESS OXFORD · LONDON · EDINBURGH · NEW YORK TORONTO · SYDNEY · PARIS · BRAUNSCHWEIG Pergamon Press Ltd., Headington Hill Hall, Oxford 4 & 5 Fitzroy Square, London W.1 Pergamon Press (Scotland) Ltd., 2 & 3 Teviot Place, Edinburgh 1 Pergamon Press Inc., Maxwell House, Fairview Park, Elmsford, New York 10523 Pergamon of Canada Ltd., 207 Queen's Quay West, Toronto 1 Pergamon Press (Aust). Pty. Ltd., 19a Boundary Street, Rushcutters Bay, N.S.W. 2011 Pergamon Press S.A.R.L., 24 rue des Ecoles, Paris 5e Vieweg & Sohn GmbH, Burgplatz 1, Braunschweig Copyright © 1970 Pergamon Press Ltd. First edition 1970 Library of Congress Catalog Card No. 69-16049 Printed in Great Britain by A. Wheaton & Co., Exeter 08 013374 6 CHAPTER 1 I CTION EVER since Bhabha and Heitler (1937) suggested that With the advent of high-speed digital computers a multiplicative processes of bremsstrahlung and pair new approach was possible. This was the direct simu­ production played a dominant role in the propagation lation of the cascade by the Monte Carlo method. of high energy electrons and photons through matter, Wilson (1952) had used hand simulation with the aid much work, both theoretical and experimental, has of a "wheel of chance". However, it requires the been done in deducing the characteristics of the cascade speed and flexibility of the digital computer to obtain produced. relatively accurate and comprehensive results. Because The theoretical work has been roughly divided into it is possible to simulate all aspects of the cascade, we two branches, one dealing with the one-dimensional can use accurate cross-sections in an exact three-dimen­ longitudinal development which considers the number sional model. Furthermore, the type of information we development of shower particles, the other with the can extract from the simulated cascade is limited only three-dimensional angular and radial spread of a by our ingenuity in programming the computer. The cascade shower as it penetrates matter. disadvantage of the computer simulation is that even In the past, two approximations, usually referred to on the fastest computers many hours are required to as approximations A and B, have been commonly used get statistically significant results. In this manner the in dealing with an electromagnetic cascade. In approxi­ simulation method is very similar to experimental mation A, full screening cross-sections are used for observations of cascades. bremsstrahlung and pair production; other processes In 1958 Messel and his collaborators commenced a are completely neglected. Ionization loss, assumed to full-scale attack on the shower problem using the be at a constant rate, is introduced for approximation digital computer SILLIAC. Results of some of this B, but no other change is made. Even in the case of early Monte Carlo work appeared in a series of five these two drastic approximations the diffusion equa­ papers, Butcher and Messel (1958, 1960), Messel et al. tions for the simplest of the number and the angular- (1962) and Crawford and Messel (1962, 1965). The radial distribution functions are of considerable results here reported are those obtained using SILLIAC complexity and their solution of such a complicated and the much faster computer KDF9. They represent nature that it is almost impossible to evaluate the results eight years of hard work, not by just the computers, numerically. A review of the early work was given by but by a group of highly skilled staff. Rossi and Griesen (1941) and a series of papers cover­ It is well known that the basic character of an electro­ ing much of the later theoretical work on the number magnetic cascade depends mainly on two types of distribution were prepared by Messel and his collabor­ interactions. When a high energy electron passes near a ators—Janossy and Messel (1950,1951), Messel (1951, nucleus there is a finite probability that a secondary 1956), Messel and Potts (1952). The angular-radial dis­ photon will be produced. Classically we say that the tribution problem likewise received much attention; electron has been accelerated in the Coulomb field of see, for instance, Green and Messel (1952), Green et al. the nucleus with the emission of electromagnetic radia­ (1952), Messel and Green (1953), Kamata and Nishi- tion. This process is called bremsstrahlung. Usually mura (1958),Chartres and Messel (1954,1955,1956), or the photon has a very small energy so that a single the review articles by Griesen (1956) and Belenki and electron will produce copious quantities of low energy Ivanenko (1960) for further references. However, in all photons as it traverses an absorber. Though the nucleus cases, there was a great lack of meaningful numerical is required to receive some energy for conservation of results, thus making the interpretation of many cosmic- momentum, it receives very little, due to its relatively ray and machine experiments difficult. large mass. The other major interaction is that of pair 2 ELECTRON-PHOTON SHOWER DISTRIBUTION FUNCTION production. Here a photon materializes into an elec­ annihilation. Here a positron annihilates an atomic tron and positron in the field of a nucleus. As in electron to produce two photons. bremsstrahlung the nucleus is required to conserve These are not the only electron or photon inter­ momentum but receives a negligible amount of actions, but they are the main ones and those which we energy. have taken into account in our calculations. The others If we consider only particles above a fixed cut-off such as the nuclear photo-electric effect, photo-meson energy we see a rapid build up in particle numbers to a production, direct pair production by electrons and maximum followed by a slower fall-off. From one high single photon positron annihilation have been left out. energy electron primary the average secondary energy All of these have negligible cross-sections, except for the decreases uniformly until it is comparable to the ther­ nuclear photo-electric effect. This may have a cross- mal electron energy. section as high as 5% (Grodstein 1957) of the total Of somewhat lesser importance are the inelastic col­ photon cross-section. However, since it occurs only in lisions between high energy electrons and the atomic a narrow range of photon energies and does not con­ electrons in the absorber. Since these collisions are tribute further electrons or photons to the cascade, extremely numerous, with very little energy transfer to we have ignored it too. We shall return to a more each atomic electron, we can consider them as pro­ detailed discussion of the cross-sections considered, in ducing a continuous energy loss. Thus we essentially Chapter 3. ignore the secondary electrons that are produced and In Chapter 2, we will discuss in some detail the subtract from the high energy electron an energy method of simulating the electron-photon cascade on proportional to its path length. To be more exact, we a digital computer. It is hoped that the description is treat only those secondaries with energy less than some sufficiently complete to enable new programs to be cut-off in this manner, and the continuous energy loss, written. we call ionization loss. The interactions with energies The results presented in this work and discussed in higher than the cut-off contribute to the total number Chapter 4 come from two programs. The first written of electrons in the cascade. These interactions are for the computer SILLIAC has been described in commonly called inelastic electron scattering. Both the Messel et al. (1962). This program used exact cross- ionization loss equation and the inelastic scattering sections for bremsstrahlung, pair production and the cross-sections are different for positrons and electrons. Compton effect. Since the low energy cut-off was 10 Photons also interact with the atomic electrons. MeV, no low energy corrections to these cross-sections Compton scattering is the collision between a photon were applied. Inelastic electron scattering was included and a free electron. We can usually consider the absor­ into the ionization loss expression. Furthermore the ber electrons to be free because the energy transfer to photo-electric effect and positron annihilation were them is much higher than their ionization potential. ignored, although exact treatment of multiple Coulomb A different type of interaction is elastic \Coulomb scattering was included. Within the range of primaries scattering. Here we consider the elastic scattering of an less than 2000 MeV and secondaries greater than 10 electron in the Coulomb field of a nucleus or of an MeV for which results are given, all of the omissions electron. Since these scatterings are quite small and cited have a negligible effect with perhaps an exception very numerous they are treated as a continuous inter­ at the 10 MeV level. action using the theory of multiple Coulomb scattering. The second program was written for a much faster Although there are angular deflections in the other computer, the English-Electric-Leo KDF9. This pro­ interactions mentioned, multiple Coulomb scattering gram includes all the low energy corrections and cross- dominates the spread of the cascade. It may be safely sections together with some very high energy correc­ ignored in light absorbers, where usually only one- tions to bremsstrahlung and pair production. As a dimensional results are required, but cannot be ignored result, it can accurately simulate cascades for any in heavy absorbers such as lead or where three-dimen­ primary energy and for secondaries as low as 1 MeV in sional results are needed. any absorber. Since this new program supersedes the Of still less importance is the photo-electric effect in SILLIAC program already described in Miessel et al. which a low energy photon transfers its energy to a K (1962), it is the only one discussed in the subsequent or L shell electron. Of similar importance is positron chapters. CHAPTER 2 SIMULATING THE ELECTRON-PHOTON CASCADE SINCE the electron-photon cascade is a stochastic pro­ where (/, m, n) are the direction cosines of the particle. cess and hence can be described completely in statistical The selection of the distance t depends on the terms, it readily lends itself to simulation on a digital cross-sections so we now consider in more detail the computer. The process of simulation involves setting representation of a cross-section as a probability up a computer model of the cascade by performing distribution and the sampling of random variates from operations which represent the motions and interac­ such a probability distribution. tions of the cascade particles. Since the correspondence The usual differential cross-section d</>(E , E E ) for 0 l9 2 between the model and the actual physical process is a a primary of energy E and secondaries of energy 0 very close one, we shall describe the model in terms of E and E = E —E may be treated as a combination x 2 Q 1 the physical processes themselves. of two probability distributions. The first is the prob­ The basis of the model is that physical cross-sections ability distribution of distance which the primary will are directly represented by probability distributions travel until it has an interaction. The second distribu­ and the use of random numbers enables us to sample tion, which is proportional to αφ(Ε , E E ), is the 0 u 2 from these distributions in order to simulate the probability of producing a secondary of energy be­ cross-sections. Techniques which use random numbers tween E and E + dE given that an interaction has 1 x x in this way to simulate statistical processes are com­ occurred. Because the probability that an interaction monly called Monte Carlo methods. will take place within a distance element dt is indepen­ The probability distributions mentioned above have dent of Mn a homogeneous absorber, the probability parameters determined by the energy of the incoming that an interaction takes place between t and t + dt is particle and the composition of the absorber. The given by particles are represented inside the computer by a set /(/) dt = φβ-φί dt of numbers giving the type, energy, weight, position in Cartesian coordinates, and orientation in direction where φ is the total cross-section. That is cosines of the particle. The absorber is regarded as a semi-infinite flat slab normal to the z-axis. The primary φ = άφ(Ε , E E ) 0 l9 2 electron or photon is injected along the z-axis. Since the control routines can only handle one particle at a where the integral is taken over all allowed secondary time any more must be stored temporarily. Whenever energies. The probability distribution for the secondary the program finds that it needs to be tracking two energies is particles it chooses to store the one with higher energy in a last-in-first-out stack. This choice ensures that the f(E) dE = (Iff) άφ(Ε , Ε E ). x x 0 19 2 maximum number of particles in the stack is less than From this equation it would appear that we need to or equal to the next integer greater than log (E /E), 2 0 calculate the total cross-section φ before we can sample where E is the largest and E the smallest particle 0 variates from this distribution. Fortunately this is not energy which can occur. The moving of the particles is necessary. Before we explain this paradox we need to done by updating the coordinates, for example, to consider the selection of random variates from statisti­ move a straight line distance / without changing direc­ cal distributions. tion the new coordinates (χ', y\ z') are given by The ability to select random variates within a digital x' = It + x, y1 = mt + y, z' = nt + z computer depends on the availability of a set of 4 ELECTRON-PHOTON SHOWER DISTRIBUTION FUNCTION random numbers. We are not interested in abstract However, by taking the larger of two random numbers concepts of randomness, but only require that the we also obtain a variate x from this distribution usually numbers shall be mutually unbiased and independent in less time than the square root would take. This of the problem at hand. Most computers now have example suggests that the design of a sampling pro­ routines which produce in practice an unlimited num­ cedure is very dependent on the idiosyncracies of the ber of random numbers one at a time. Each number required distribution. There is a method which is a depends uniquely but in a very obscure way upon its combination of "the composition method" and "the predecessors. By using the same starting values the rejection methods", both described in Butler (1956), sequence may be repeated—a facility which is of con­ which is of considerable power. siderable value in code checking a program. In actual If f(x) can be written production runs care is taken not to repeat identical sequences. We used a method of generating random n numbers due to Coveyou (1960) and tested by Ruehn Ax) = /*ift(x)glx) t (1961). This method provides random uniform num­ bers, within the range 0 < ξ < 1. The symbol ξ will always be used to denote such a variate. where a, > 0 / = 1, 2, . . ., n Let us consider the frequency distribution f(x) dx 0 ^ g (x) < 1 with Cumulative frequency distribution F(x) i.e. t 9 X ft(x) > 0 for all x F(x) = J7(x) dx. and fi(x) dx = 1 0 A theorem which makes it possible in principle to write down a rule for computing variates from any then a random variate x may be chosen by distribution is that the cumulative distribution F(x) is itself distributed uniformly. If x is sampled from/(x), (a) select a random integer / (1 < / ^ n) with the probability that x will be less than xf is F(x'), and probability of selecting / being proportional to since F(x) is a monotonic increasing function of x we have (b) select a variate x' from the frequency distribu­ tion/,(*), Prob [F(x) < F(x')] = Prob [x < x'] (c) calculate gi(x') and accept x = x' with prob­ = F(*'). ability gi(x')9 if rejected repeat from step (a). Therefore one method of sampling x is to compute x The value of the method lies in the fact that a de­ from composition of the frequency function can usually be F(x) = ξ 0 ^ ξ < 1 found where n is a small number, the distributions ft(x) are easily sampled, and gi(x) is never much less than one, or x = F-1 (0. this means that a rejection is a rare event. It is of in­ For example if terest to note that the probability of accepting any trial is F(x) = 1 — exp (—x/x) n then x = — x In (1 — ξ) 72- = x In ξ. The last step is possible because 1 — ξ is a uniform Thus the average number of attempts is variate with the same limits as ξ. This example gives us the most useful method of sampling from the exponential distribution. However, this method is not much help when the cumulative distribution does not have a simple inverse and even when it has, some other <=1 methods may be better. For instance to sample from Examples of distributions easily sampled are those the distribution which have simple inverses and those which have the f(x) dx = 2xdx 0 < x < 1 form the inverse method would have us take f(x) = (M + a + l)!^ (i _ y o ^^\ x x ml n\ SIMULATING THE ELECTRON-PHOTON CASCADE 5 where m and n are positive integers. To sample x we we can avoid the calculation of the total cross-section select m + n + 1 random numbers and order them, φ since we may use 9 i.e. n αι 2 £l < £2 ^ ?8 · · · ^ im+if+l then we select for x the number ξ„ . +1 instead. Then whenever a variate is rejected we As an example of the use of this sampling method sample a new distance and move the particle before and because it is of general interest let us consider the another variate is sampled. Thus the particle may be normal distribution moved several times before a successful interaction is simulated. /(*) ■Ae ~x2/2 x>0. We will now prove that this gives the correct cross- section. Suppose that the correct total cross-section is φ and that We need only consider the reduced form and positive values as it is a trivial matter after we have a sample variate to perform a scale change and provide a ran­ /*t = Φ\ dom sign. A decomposition due to Butcher (Thesis) which is very efficient is then clearly the probability of accepting a trial is φ/φ'. =J\ Thus if k attempts are made before acceptance, the /w 1 -*2/2 distance t travelled will be distributed as (ΦΎ -f- —- 2 e~2ix~1} £-(*-2)2/2 -ΦΊ V27T " (k - 1)! where But the probability of having exactly k attempts is {ΦΙΦ'ΧΙ—ΦΙΦ'Υ-1. Hence the distance travelled will be - =J! 1 distributed as > 0 00 Μχ) = 1 Σ (<L·)l·tk-1e-''", 6 W' e Σ. (1 - φ/φγ- (x) = e-*i* gl (k-iy. φ' and "Σ <f>e~ 1 a = — 2 V277 /,(*) =2e-2"-« > JC ^ 1. = φ e -4>t g2(x) = e-«*-«2/* J which is the correct distribution. The method is readily generalized to the case where there are two or more In this case the decomposition corresponds to two competing interactions. 3 ranges of x. The value of a + a is ,— ~ 1.2 which In considering a particular cross-section it may well x 2 be that the decomposition used has values of is the average number of trials which must be made. It will be noted that this method of generating random na i 2 normal deviates is exact within the limitations and accuracies of the computation. We now come to a point which is of considerable value in simulating physical cross-sections. If we ex­ dependent on the primary energy. In this case care press the differential cross-section in the form must be taken if the primary is continuously degraded in energy by a process such as ionization loss. Further Σn care is necessary if one is dealing with an inhomogen- <**/*(» giM eous absorber. A useful technique is to introduce a pseudo cross-section which does nothing except reduce 6 ELECTRON-PHOTON SHOWER DISTRIBUTION FUNCTION the average step length. Whenever this pseudo cross- error is that position of the terminal point may be section is selected the program immediately returns to slightly wrong. Furthermore, it is in just this low energy move another step and in so doing recalculates region that limitations on the maximum distance t are required for multiple Coulomb scatterings. Thus we have used only the simple form for calculating ioniza­ n tion loss. It should be noted however that this simpli­ fication is not necessarily valid in the general case. i= 1 The other interaction which is best dealt with as a In the present program because a limit has been placed continuous process is elastic Coulomb scattering of the on the maximum distance δ, which electrons may electron in the field of the nucleus. It is possible to move, this technique has not been used. When a dis­ simulate these scatterings directly as normal cross- tance t is sampled the electron is moved in steps of δ sections. However, such a scheme would be prohibit­ and then the remaining distance (less than δ) to give ively expensive because of the large cross-sections a total distance t. The reason for introducing a maxi­ involved, and since adequate theories are available mum step δ will be returned to later in the discussion which predict the angular distribution of the scattered on multiple Coulomb scattering. electron after a path length t, we have adopted this Not all interactions are conveniently represented as approach. Given that the electron with position co­ cross-sections. Ionization loss and multiple Coulomb ordinates (x, y, z) and direction cosines (/, m n) is to 9 scattering are best simulated as continuous functions be moved a distance /, we move this distance in its old of the electron track length. In general the rate of direction and then sample a spatial angle Θ through energy loss per track length may be expressed as which it is scattered. The distribution of Θ depends on the electron energy and on the distance t. The dt angle 0 is measured from the current direction of the electron. We now have to sample a random azimuthal where the function/(is) depends only on the energy E. angle and then calculate the new direction cosines. Now provided the distance t is small the energy loss Let μ be the original direction of the electron and Δ£ incurred by an electron of initial energy E is 0 μ' = (/', m' ri) be the direction after scattering. Then approximately 9 if a and β are two unit vectors which form an ortho­ gonal triad with μ we have μ' = μ cos© + (Ca + Sß)s'm0, The error in using this approximation may be esti­ where C and S are the cosine and sine of a random mated from the more accurate expression angle. These may be found easily by using a method suggested by von Neumann (1951). Select a pair of Kdt/Eol 2\dE dtj* \ random uniform variates ξ and ξ such that 0 χ 2 Now as will be seen later the ionization loss can be fi2 + f.1 < 1 expressed by then _ ii2 ~ &' c fi2 + f.1 where energies are in mc2 units, distances are in radia­ and tion lengths and typically b ~ \a and γ ~ J. The correction term in this case becomes \ybt E-v-i 0 where S is given an arbitrary sign. The most conven­ which is negligible at high energies. At low energies we ient forms for a and β that have been found are can show that the correction is less than « = ( - ^ - - 1 , ^ , 1) \n + 1 /i+l / l Im m2 \ This result follows from the observation that the maxi­ βQ = , — 1Λ, /w 1. mum distance that the electron can travel is that which would reduce its energy to zero. Obviously the error is Because of ionization loss we must allow for the a maximum at low energies where the required accur­ change in energy of the electron as it traverses the acy is least. In this region the only result of such distance t. We do this by replacing E2 by E E, β2 by 0 SIMULATING THE ELECTRON-PHOTON CASCADE 7 ßß, etc., where E and β are the initial and £and ß the results. For 5 MeV electrons the correction to the path 0 0 0 final energies and velocities respectively. This substitu­ length for an average step is only 5% and is much tion will give us the correct mean square scattering smaller for high energy electrons. dE There is one further complication to the moving of angle if the rate of energy loss, — is constant (see particles and this is because we need to get information dt out of the program. As previously mentioned we con­ Rossi, 1952, p. 68). A source of error results from the sider the absorber to be a semi-infinite horizontal flat assumption that all the scattering takes place at the end slab with the primary injected vertically to the surface. of the track. This error is not at all serious provided We then count the number of secondaries as they pass the scattering angle is small. Similarly the lateral dis­ through a set of horizontal levels at regular depths in placement due to scattering has been neglected. Both the absorber. For complete tabulation we note the these errors are negligible if the maximum step length exact type, energy, radial distance and angle of each is kept small enough at low energies where scattering secondary that traverses each level. The radial distance is greatest. is measured from the core of the cascade, defined as the A related effect has been included in the simulation extrapolation of the primary track, and its angle is program. This effect is the increase in path length over measured relative to the primary direction. There is the straight line distance due to multiple Coulomb no need for any other spatial or angular measurements scattering. It has been shown by Yang (1951) that if t as theory predicts complete rotational symmetry. is the total distance travelled, it is related to the straight To obtain the required data for each secondary the line distance s by simulation program must note whenever a particle would cross a level. Thus every time a particle is moved, t = + i S\t) dt the distance (along the particle's direction) to the next s level is calculated and if the particle would cross the level it is first moved to the level, recorded and then where 0\t) is the mean square angle of scattering and moved the remaining distance. It is of interest to note is a function of the distance t. Since we are only estima­ that because of the exponential distribution, we could ting a correction we may use a rough estimate for quite validly forget the remaining distance and re- 02(f). Following Rossi (1952, p. 68) we have sample a new path length. However, it is usually faster to remember the remaining distance. W) =— t 9 So far no mention has been made of particles which ß*E2 are travelling backwards. There is no trouble in simu­ where E is the scattering energy, independent of lating these particles provided we do not wish to record s absorber if t is measured in radiation lengths and is them. However, once we introduce levels there are equal to 42 mc2. On integrating we get complications. Since a particle may circle around and cross a level several times, a decision has to be made about how to record them. The decision adopted was to \β*Ε) track all particles in the backwards direction until they had crossed a level, after being recorded they are or tracked no further. This decision it is felt corresponds most closely to experimental situations. For instance, L 4 \ß2Ej J in a multiplate cloud chamber, consider one of the gaps. The program would simulate all forward going This equation forms the basis for our limitations on the electrons coming out of the top plate and all backward maximum step length allowed as mentioned earlier. going electrons coming out of the bottom plate, but We require that the bracketed expression shall always not any electron which emerged from the bottom plate be greater than \. This gives the requirement entered the top plate and then re-emerged in the for­ ward direction. Not only is the number of such elec­ trons very small but in general their numbers would be altered by the intervening absorber. A further conse­ Since the lowest energy to be considered is 1 MeV ~ 2 quence of our treatment is that backwards going parti­ mc2, the smallest value of t is 0.001 radiation lengths. cles do not enter a plate from below and emerge from m Even this expression for t„, which gives a root mean . its top surface. The results of the simulation will then square angle of scattering of approximately 80° is too tabulate at each level the number of particles as a large for all the approximations made. But since these function of Θ, their angle to the primary direction. very low energy electrons remain in quite a small Forward going particles have 0 < Θ < 90° and back­ region until they lose all their energy no serious error ward going particles which come from the absorber 8 ELECTRON-PHOTON SHOWER DISTRIBUTION FUNCTION below the level have 90° ^ Θ ^ 180°. The radial and factors involved. To prevent large fluctuations which energy distributions are given only for forward going could arise if one particle achieved a very large weight particles. Track lengths and energy losses are tabulated we limited the maximum weight to 8. Once a particle every time a particle moves, and refer to the absorber achieved this weight it was no longer subject to the between two levels, hence backward going particles are sampling scheme. included. One necessary requirement of any modification to One of the problems with direct simulation of the the direct simulation of the cascade is that it does not electron photon cascade is that while a large number of introduce any bias in the final results. An essential part particles occur near the cascade maximum and hence of our importance sampling scheme is that the prob­ results for this region have high statistical accuracy abilities for duplication and rejection are fixed and that there are many fewer in the cascade tail with low statis­ each sampling process is completely independent of all tical accuracy. We would like to have relatively the others. This means that we only need consider a single same statistical accuracy for all results derived from sampling process in order to see if there is any bias. the simulation. Since the number of particles going into Since we are mostly interested in energy and number the many cells of the radial and angular distributions averages all we need to show for no bias in these cases are both highly variable and mutually correlated we is that averages taken immediately after a level have the shall consider only what can be done about the same expectations as those taken before. Because the one-dimensional distribution. What we would like is scheme does not alter the individual energies, positions to simulate fewer particles at the cascade maximum and or angles of the particles the averages will still be put more in the cascade tail. Furthermore we would like into the correct distribution cells. For the high energy to simulate more high energy particles and fewer low duplication scheme it is apparent that the before and energy particles. As a rather crude attempt to achieve after averages are in fact identical. Therefore this part these aims and save computer time a scheme of impor­ of the scheme does not introduce any bias. For the low tance sampling has been implemented for the KDF9 energy rejection scheme the two averages also have portion of our calculations. the same expectation. This was achieved by dividing This importance sampling scheme gave each particle the weight of surviving particles by their survival a weight which could only be altered when the particle probability. crossed a recording level. By correct control of the The effect that the importance sampling scheme has particle weights we can either increase or decrease the on the statistical accuracy of the results has to be actual number of particles simulated but still get correct considered. Except for the first few levels where the estimates of the average energies and numbers. The scheme has little effect its main result is to increase the scheme makes a distinction between high energy and number of high energy particles simulated and to low energy particles; only high energy particles may be decrease the number of low energy particles simulated. duplicated and low energy particles may be retained or But since the low energy particles are the products of rejected but not duplicated. We have taken the demar- the many high energy collisions it can happen that kation energy as one tenth of the primary energy. Two there is an overall increase in the number of particles preset parameters p and p control the operation of simulated compared to cascades in which the sampling x 2 the scheme. The parameter ρ is the probability that a scheme is not used. We shall return to this point in Ύ high energy particle will be duplicated on traversing more detail in Chapter 4 in the discussion of errors. a level. The duplication is done by making an identical We will also see in Chapter 4 one disadvantage of the copy of the particle in the current particle stack and importance sampling scheme: we can no longer have giving to each one, half the weight of the original an exact accounting of the energy distribution. If a particle. For low energy particles the parameter p is greater than average number of low energy particles 2 the probability that the particle would be allowed to survive it is possible for there to be more energy carried continue past the level, in which case its weight was by the total of particles than the original primary divided by p . Particles which failed this selection were energy. Thus at a given level for p = 1/2 it would 2 2 rejected by removing them from the current particle mean that more than one half of the particles with stack. Because of the cumulative properties of the E < 0.1 E had survived. Since these particles' weights 0 duplication scheme at successive levels, the time taken are all greater than one, they would contribute more to simulate a cascade is a very sensitive function of the than the original total energy of the low energy particles, duplication probability p. We chose the values p = even though as noted previously the average energy x x 0.2 and p = 0.5 as a reasonable compromise of all expectations still remain the same. 2

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