Calhoun: The NPS Institutional Archive DSpace Repository Theses and Dissertations Thesis and Dissertation Collection 1966-05 Elastic scattering of low-energy electrons from oxygen Johnson, William Lewis http://hdl.handle.net/10945/9495 Downloaded from NPS Archive: Calhoun NPS ARCHIVE 1966 JOHNSON, W. m mm MSB m ill 88$ :>;.':-,•;, ,,;,' lilii ,giSHii HB OF LOW-ENERGY ELECTRONS FROM OXYGEN .ASTIC SCATTERING JOHNSON la— ffl$3QOT§al» M lialiilfS Smmm H|^Hn JHBi nsiiiiHg WffiKHfl WW! LIBRARY NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIF. 93940 for publio This document has been approved is unlink distribution .release and Eale; its '£/ ELASTIC SCATTERING OF LOW-ENERGY ELECTRONS FROM OXYGEN by William L. Johnson Lieutenant, United States Naval Reserve B„A,, University of Southern Mississippi, 1962 Submitted in partial fulfillment for the degree of MASTER OF SCIENCE IN PHYSICS from the UNITED STATES NAVAL POSTGRADUATE SCHOOL May 1966 MPs A<2£t*we The cross sections for the elastic scattering of electrons from atomic oxygen are calculated in the energy range between electron volts. and 13.6 Polarization of the atom is included by using a term in the potential function which has the correct asymptotic behavior and which vanishes at the origin. results are discussed. Previous theoretical and experimental CI- TABLE OF CONTENTS Title Section Page 1. Introduction 5 2. Review of the partial wave method for computing the cross section 7 3. Potential function used for electron-oxygen scattering 10 4. Numerical methods 15 5. Previous calculations and experimental data 19 6. Results 22 7. Conclusions and Acknowledgements 23 8. Bibliography 24 LIST OF ILLUSTRATIONS AND TABLES Figure Page 1. Radial Charge Density of Oxygen 26 2. Behaviour of the Core Potential near the Origin 27 3. Polarization Potential with q = 5 28 4. Polarization Potential with q = 8 29 5. Cross Sections with ex = 30 6. Cross Sections with ex = 5.5 7 Theoretical Cross Sections 32 8. Experimental Cross Sections 33 1. Results of Calculation for ex = 5.5 34 2. Results of Calculation for ex = 6.0 35 3. Results of Calculation for ex = 36 and 6 31 Table 4- 1. Introduction. A knowledge of the elastic scattering cross sections for electron- oxygen collisions is of practical importance in the study of the properties of air at high temperatures. The experimental determination of low-energy cross sections is especially difficult in the case of atomic oxygen because it recombines easily to form molecular oxygen. Only re- cently have experiments been done to measure this cross section in the energy range below 15 electron volts. [11,15] retical treatments have been made. Several previous theo- [1,3,7,9,12,16] The results are divergent, and none agrees satisfactorily with the experiments. The elastic scattering of low-energy electrons by neutral oxygen is treated here using the partial-wave method of Faxen and Holtzmark.[ 13] This method, which is outlined in the next section, allows one to de- termine the cross section if the potential field in which the electron finds itself is known. The first approximation to the scattering treats the atom as a positive charge at r = metric negative charge distribution. surrounded by a spherically symThe charge density of this elec- tronic distribution is calculated from the Hartree wave functions for oxygen This first approximation is inadequate because it ignores the dis- tortion of the atomic electron distribution by the Coulomb field of the incoming electron. This polarization effect is included in this calcu- lation by representing it with a polarization potential in addition to the undistorted potential. The polarization potential can be thought of as the term which represents the difference between the true interaction potential and the undistorted potential. The form it assumes for large separations is known; for small separations the form is uncertain and will be discussed further in Section 3. When the incident electron is within the electron cloud of the atom there is an additional repulsive force due to the Pauli principle. Hammer ling, Shine, and Kivel have treated this exchange effect by the inclusion of a third potential to approximate the change in the electron's energy due to the deficiency of electrons with like spin near it. [7] Such an approximation is similar to Slater's treatment of exchange in atomic wave function calculations. The result of their cross section calculation which includes this approximation shows that the exchange effect makes a negligible contribution to the cross section in the energy range considered here. Furthermore our polarization potential will have a parameter which is adjusted to fit experimental data. The value of this parameter is affected by the exchange contribution, so no specific account is taken of the exchange potential in this calculation. The actual evaluation of the cross sections using the phase shift method involves using a computer to integrate numerically. Schroedinger 's equation The details of the procedure are given in Section 4. The following atomic units are used: unit of mass = m = rest mass of the electron unit of charge = e = unit of length = a charge of the proton in Gaussian units = h 2 2 /4tt 2 me =radius of the first Bohr orbit 2 Consistent with these, the unit of energy is e /a , which is twice the ionization energy of hydrogen and the unit of angular momentum is h/2rr. It should be noted that one atomic energy unit equals about 27.2 electron volts; this is twice the value of another commonly used unit, which is 13.6 ev. the rydberg, 2. Review of the partial wave method for computing the cross section. The scattering of two bodies when considered in the center of mass system is equivalent to the scattering of a single particle with the reFor the electron-atom problem the duced mass from a potential, V(r). reduced mass is very nearly equal to the mass of the electron. In this case the center of mass frame is identical to the lab frame. Since the potential function, V(r), is assumed to be spherically symmetric, the electron's wave function may be separated and written as -2 Y(r,0) In atomic units R.(r), the radial wave function, satisfies the equation ^- A_ -1 dr 2 RjCr) P^ (cos 0). + [2E 2V(r) - 4i*±U - ] J R (r) « o. ^ a, beyond which V(r) If we assume that there is a distance, r is zero, equation (1) may be solved exactly in the region r > a, giving R^r) = A^ [cos ^j^Ckr) - sin 6 £ n^(kr) (2) ], where A. and 6. are constants of integration, j. and n. are the spherical =V2E. Bessel and Neumann functions, respectively, and k The asymptotic form of equation (2) is A > V r) ~ 2 [sin (kr kr~ " * lTJ + V ] ' so that > Y (r,9) ~ 2 P (cos £ 0) H ~- [sin (kr Ju •7- - \ Xtt + b J ]. (3) The physical meaning of 6. may be seen by realizing that if there had been no potential anywhere, the asymptotic form of R. — — sin (kr - \ 4tt) (r) would be Hence 6., the phase shift angle, is the quantity . which describes the scattering. In a symmetrical scattering situation we expect an asymptotic wave function to be in the form of a plane wave superimposed on a spherical If the plane wave propagation is in the scattered wave. z direction, we express the asymptotic form of the wave function as Y~ ikz e +1 r f( 9 ) Since the asymptotic form of e i k-z e ikr . is 00 ikz e ~ „ S 4=0 .4 i ... _ sin (kr-%* (24+1)s P. t(cos 9)s *r kr * 4rr ) , the asymptotic scattered wave function may be written as Y ~ i\u 2 +1) P,(cos 0) 8ln * 1=0 < kr kr ^ *n ) + f(e)e ikr . (4) Equating (3) and (4), writing the sine function in exponential form, and solving for f(9), we get 00 f(9) E =ttZlk + l)(e 2i6i -l) P,(cos (24 * 4=0 9) . The differential scattering cross section is f=|f(9)| 2 . Integrating this over all solid angles, we get the total cross section 00 a E -f§k (24 + 1) 4=0 8- sinVl . (5) The value of 6. will be very small for i > ka, so that for the range of energies considered here values of & greater than 2 or 3 need not be considered in calculating the cross section from equation Hence in order to find a, we need the values of 6 . 5. These are i found by solving the wave equation (1) numerically to evaluate R«(r) and its derivative at r = a. at r = a from equation (2). R*(r) and its derivative are evaluated These two wave functions are matched at the distance a by equating the logarithmic derivatives. the values of the phase shift angles, 6.. This gives When all significant phase shift angles have been calculated, equation (5) is used to evaluate the cross section at the given value of energy. This process is repeated over the energy range of interest to find the spectrum of cross sections versus energy. Potential function for electron- oxygen scattering. 3 A calculation of the electron- oxygen elastic scattering cross section is routine, although tedious, if V(r) is known and a computer is available. In this calculation we assume V(r) is the sum of the undistorted atomic potential, V„(r), and the "polarization" potential, n V (r), which attempts to represent the difference between the true po- tential and the undistorted potential. V„(r) may be found in a direct electrostatic manner if the electron n. charge distribution is known. [14] The charge distribution is calculated from the Hartree wave functions of the oxygen electrons. Hartree approximation treats each atomic electron Since the as moving in a spheri- cally symmetric potential, the atomic electron wave functions can be written as U =R n/ r )Y ' ni m e m (9 '- '>' where Y. (0',0') are the normalized spherical harmonics. The values of j&m R . (r 1 ) have been tabulated by Hartree. [8] In computing the electron * volume charge density one sums UU for each electron. For filled n,jfc shells this sum will be spherically symmetric; the only asymmetry will be contributed by the outer shell which is not filled. Hartree approximation to neglect this asymmetry. It is within the Hence the charge density of electrons is given by ^'>= S N nX n,i where N 3 „ nX R L (r '> P ground state of oxygen is considered here, and N Only the represents the number of electrons in the n,Z shell. =4, -10- for which N 10 = 2, ' N 20 = 2, V (r) consists of a negative term due to the nucleus and a posirl tive term due to the electron cloud. =° „(,).. H i + f r 2rr tt [2R (r') + 2R ~ [ f J J J - V " [p 2 - 4R^(r') 1 .,..,.„., r' sin 0' dO'dfl'dr' r' ^(r'), Letting r'R^Cr') = - (r') + — r „ may be written as It ( -^ r «) + p 2 (r')+ 2P 2 (r 1 ) 1 ^-Tn dr . The integration can be divided into the contribution of the electrons and r' = r, and the contribution of those from r' = r between r' = to r' =». may be written as Then V rl Vu (r) = H - *8 + r 8tt r f [P 10 —& (r )+ P ' / ' )+ 2P ^ (r,) ] 21 dr' (6) r J J +8n r ^ (r 20 [ p io 2 (r, N . P .(r The function S n* nX n,Z > 1 ) > +p ? ,)+2p ^ r '> i is called the radial charge density. It . represents the probability per unit length of finding an electron in the spherical shell between r' and r 1 + dr ' . Figure 1 is a graph of this function for oxygen. The treatment of the polarization potential is less exact. The pro- cess of treating the atomic potential as the superposition of an undis- torted potential and a polarized dipole potential is less than rigorous. -11- However, even if we accept this approach, the form of the polarization potential, V_(r), is not certain. If the incoming electron is at large r, its electrostatic field at the atom is nearly homogeneous and has a value of 1/r 2 . This field in- duces a dipole moment which is directly proportional to the field, M< = a /r 2 , where a is the polarizability . This dipole moment then exerts an attractive force back on the electron with a value of So, f = 2p«/r 3 = 2a/r for large r, V n (r) - - f 2a/r 5 dr = This form of V (r) for large r must be modified so that the function does not blow up at the origin. At the origin there should be no polari- zation force since, in this limit, spherical symmetry prevails and no multipole moments can be induced. For this reason the proper polari- zation potential should have the property that _d Limit r - dr P ( vw m When the scattering electron comes "inside" the atom, the atomic electrons still tend to hide behind the nucleus. asymmetry gives rise to a repulsive force. However in this case the In this classical picture, the polarization potential should also have zero slope at a value of r which is characteristic of the size of the atom. A function which satisfies these conditions and which will be used in this calculation is V (r) p - •£$ 1 - ( -12- exp [- (r/r q Q ) ] . ] (7) 5 This function, with q equal either five or eight, was first used by Biermann to account for polarization in the calculation of oscillator Garrett and Mann have used this polarization potential, line strengths. [2] with q calculations of electron scattering from alkali atoms. [5,6] 8 in They obtained good agreement with experimental scattering data by treating a and r Graphs of equation as parameters. 7 are given in Figures 3 and 4. The exponential in equation (7) may be expanded so that for, small r we have — dr V (r) K J ? oc r-0 r^" 5 From this we see that the requirement that the polarization force vanish at the origin restricts q to be greater than 5. In this calculation we The result with q = 5 represents a use values of 5, 6, and 8 for q. limit since any value of q larger than five satisfies the condition mentioned above. is taken to be the The value of r of the valance electron shell. expectation value of the radius Its value is calculated from the Hartree wave function for the outer shell as follows 00 = : ° This yields r o / r« Jo =1.2 atomic P^(r') dr'. 21 units, No direct experimental values of the polarizability are available. Several calculations based on indirect experiments have been made. Klein and Brueckner found a to be 5.589 by adjusting it to give the correct binding energy for . [9] Using a similar procedure, Cooper and Martin calculate a value of 5.499. [3] Both these methods do not attempt to provide the true polarizability of the atom, but yield a number which -13- includes exchange and other effects. Dalgarno and Parkinson found a value of 6.005 based on experimental determinations of the dielectric constant. [41J In our treatment r o is fixed and a is taken to be either 5.5 or 6.0, and for both of these values the cross section is computed for q = 5, 6, and 8. 14- 4. Numerical Methods. Before the wave equation can be integrated it is necessary to know V (r) H This function was calculated from equation (6) using a trapizodial . found that the resulting function could be It was summation technique. fitted closely by 2 1 V (r) = H - ^~ IVf-^— +Y 2 8 where + Y 3 -A r r -A. + Y 4 e v = 1.2806 y k = 2.2376 X e , = -0.2806 2 = 18.263 Y 3 = 3.0715 y 4 = -1.9710 X- = 6.803 X, 4 3 ] = 11.548. This functional form was much easier to enter into the computer than tabulated data points, and the fitted function matches the computed *» function the fifth significant figure. To solve equation (1) the substitution Y.(r) = r R.(r) was made, yielding the equation d \ dr (r) \ = M 1(1 * + [ 1) l) | + 2V r R + 2V (r) p (r) - 2E ] Y (r). Equation (8) was integrated using a Runge-Kutta approximation. to use such a (8) In order method it is necessary to know an initial value of both Y and dY/dr at some starting point. These values were found by assuming a solution 00 Y (r) s - v a S C r _ n=0 n -15- n , = C ' o 1. Since this solution will be used at a small value of r, a series approxi- mation for V (r) and V may be used in equation (8). (r) Neglecting terms or smaller, we have in r V (r) R + b + b b /r Q <* x r, 2 where = 8 b Q b ( Yl + y 2 ) =8; y^ = 8 (- b x - Y 2^ 2 + Y 3 + Y4 ) ! = 8 2 Also for small r, V «a —o/— r q-4 Only for q = . 5 will this make a con- tribution to the total potential in the above approximation, changing the — a + given above to b value of b 1 Equation (8) for small , r, becomes 2r o r - T* dr i(X + 1) + 2(b + r indical equation 1 c So = + 2E b r into equation = Z(Z + 1). 1) 2 r ) =0. Y 2T b C n-l l ~ 8 - we get the The only acceptable root is +(b l +E)C n-2 +b 2 C n-. n(n + + (8'), The recursion relation is n A „/% Y (r)^r s o/(a - since Y(0) = 0. C + s Substituting the series solution for Y a = i + 2 b r r U 4+2 l 16- + 1 1) — dY (r) , and s m , ,_> f (l+l)r 8U+2) + Sff* X. t A+l (8') One could, of course, evaluate these equations at = r and start the integration from there, however it was found that the accuracy of the Runge-Kutta integration approximation is very sensitive to the step For this reason we evaluate Y size chosen near the origin. and dY /dr s s at r = .01 and use these values to start the iteration procedure. The step size was determined by choosing an arbitrary value to do a trial calculation, reducing the step size and repeating the calculation until there was no significant difference between two successive results. A Although this value is smaller than needed step size of .002 was used. for large r, no attempt was made to change the step size as the iteration progressed Equation (8) was integrated to the final point r = a which was determined by the condition V — — + V (a) (a) ^ E For r > a (2) _ 4 = 10 we have a region of almost zero potential, so from equation the solution of the wave equation is V r) = V t cos b ih^ kr) " sin 6 n (kr) x 4 1 • The derivative is dY>(r) : = A„r r i 2iVr / [Xj x-i (kr) - -[in^Ckr) w - + (i u W + l)n i+1 kr) i cos 6 « r) (kr) ]sin 6 \ + Letting Y^(a) and Y^ (a) denote the computed values of Y, (r) and 17- V — at r = a, we equate logarithmetic derivatives at r = a to get dr Y^'(a) T Y^(a) k = (22+l)[cos 6^ ^(ka^sin ^(ka)] 6 ( -[jen _ x 1 (ka)-(X+l)n (ka)]sin6 j6+1 i l4 Solving for 6. gives tf'Ca) '(ufr V 6 . *W"> w+d^+iO") - ) -777 Y„(a) V + ka) ] / V ka) = arctan (9) Y,(a) a (2^ ^.l (ka) " Ci+Dn1+l (k.) ] C n -J— Y,(a) <ka)] + n (ka) ) From equation (9), for a given I and E, a principle value of 6. is found, For any E, value of a this process is repeated for I is found from equation (5) . =0, 1, 2, Then the and 3. As expected the contribution to the cross section from the Z = 3 term is negligible in the energy range considered. The entire calculation was done for energies between steps of .05 for q =5, 6, and .50 in and 8; and for & = 0, 5.5 and 6.0. putations were done on a C.D.C. 1604 computer using Fortran-60. All comThe com- putation time for each run (a given q and a) was about four hours. This large amount of computer time could be reduced by increasing the step size at large values of r. 18- Previous calculations and experimental data. 5. The theoretical treatments of the low-energy scattering problem One approach is similar to the one may be divided into two groups. used here, but different forms of the polarization potential are used. The other treatment is much more elaborate. It attempts to solve the Hartree-Fock equations of the system of scattered electron plus atom. Figure 7 shows some results of previous calculations. Robinson uses no polarization potential. [12] is calculated from His potential function Hartree-Fock wave functions, and the cross sections calculated by the partial-wave method for I = and 1. He also evaluated the cross sections using the W.K.B. approximation and showed that it leads to very large cross sections at low energies. Klein and Brueckner also treat the problem using the partial-wave They account for polarization with the potential method. [9] V„(r) = P 2(r 2 o + 2 x V2 This potential function has been used often in the treatment of polari- zation in atomic wave function calculations. It gives a zero polarization force at the origin, but differs from the function used here (equation 7) in that it produces an attractive force for all r. As mentioned before, they determined the polarizability from experimental data on the binding energy of 1) . . Their curve in Figure 7 includes s and p waves (i = and Cooper and Martin [3] found a mistake in the paper by Klein and Brueckner. They use the same procedure and arrive at cross sections which show a decrease at low energies -19- Hammerling, Shine, and Kivel treat polarization in the same way as Klein and Brueckner. meter. [7] They take o/ = 5.4 and r as an adjustable para- They also include a term in the total potential to represent the exchange energy. This term varies as 1/r the Slater approximation. 3/2 and is derived from ' They show results obtained by neglecting both polarization and exchange, and neglecting polarization only. The cross sections obtained by using just the Hartree potential are different from any obtained previously. The cross sections with exchange and polari- zation are plotted in Figure 7 . It is not clear why these should be so different from the other calculations since they reported using the same method. Temkin includes polarization effects within the Hartree-Fock formalism. [16] He associates with each atomic electron's wave function a polarized part which depends on the coordinate of the scattered elec- The wave function of the scattered electron is made antisymmetric tron. with respect to the total atomic wave function. This gives rise to the kind of polarization potential considered here, called direct polarization, and another term, called exchange polarization, which contributes about 15% to the cross section. shown in Figure 7. His results for s-wave scattering are Bauer and Browne have modified Temkin 's method. [ l] They made more drastic simplifications in the Hartree-Fock equations and are able to calculate s, p, and d-wave scattering. Their cross sections are small at low energies and fairly flat at higher energies. The most accurate experimental data is that of Neynaber, et al. [ll] They have measured the cross sections in the energy range from about to .45 (2.3 to 11.6 eV) . .1 They find the cross section to be almost constant •20- at 19.5 + 1.3 throughout the energy range. half of their 64 experimental points fall. This represents a band in which Sunshine, Aubrey, and Bederson measured the cross sections between about .03 and .45. [15] There is more scatter in their data, but there is general agreement between the two experiments. Lin and Kivel obtained a low energy point at about .02 energy units using a shock tube. [10] If this point is accurate it in- dicates that the cross section decreases sharply at low energies. Al- though these experiments are extremely difficult and have low precision, they do indicate the magnitude of the cross section and show its general dependence on energy -21- Results. 6. The numerical results of our calculation are given in Tables and and summarized in Figures 3 and 6. 5 The curve labeled a = 1, 2, repre- sents the cross sections obtained by ignoring the polarization potential. This curve corresponds almost exactly to that of Robinson. that the differences between Hartree - This indicates Fock wave functions used by him and Hartree wave functions used here have an insignificant effect on the cross section. The introduction of the polarization potential increases the phase shift angles but decreases the cross section. The smaller values of q produce potentials which give rise to smaller cross sections, and also straighten the curve out. The remarkable feature indicated by Neynaber's experimental results is the almost constant value of the cross section between .1 and .45 energy units, in this energy range. value [ll] Our results give a similar constant Further, the measurement of Lin and Kivel gives evidence that the cross section has a very small value at the lowest energies. [ 10] This is also a property of our results. Of all the theoretical calculations that have been discussed, that of Bauer and Brown is the most pure (not dependent of experimental para- meters) which extends of the entire energy range, [l] with <y = 6 and q = 6 almost duplicates their results. Our calculation Our results are also consistent with those of Temkin at the lowest energies. [16] 22- 7. Conclusions and acknowledgements. No attempt has been made to justify the fundamental validity of the form of the polarization potential except in a general way. Experi- ments indicate that consideration of polarization in any scattering calculation is important. Although the "correct" way to treat the effect has been outlined by Temkin, it is desirable to have a more tractable Our results indicate that the potential semi-phenomenological method. function used here (equations 6 and 7) with <x = 6 and q = 5 gives cross sections which have the energy dependence indicated by experiment and by the more exact calculations. Our results seem much more realistic than previous treatments using other forms of the polarization potential, The author would like to thank Professor William B. Zeleny for suggesting this subject as a thesis topic. The help provided by the staff of the Computer Facility of the Naval Postgraduate School is greatly appreciated. -23- BIBLIOGRAPHY 1. Bauer, E. and H.N. Browne. Elastic scattering of electrons by the many-electron atom. 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Journal of Applied Physics v. 28, July 1957: 760 - 764. . , 8. Self-consistent field, Hartree, D.R., W. Hartree, and B. Swirles. including exchange and superposition of configurations, with some Philosophical Transactions of the Royal Society results for oxygen. of London v. A238, 1939: 229 - 246. , 9. and K.A. Brueckner Interaction of slow electrons with Klein, M.M. Physical Review v. Ill, atomic oxygen and atomic nitrogen. 15 August 1958: 1115 - 1120. , , , 10. Lin, S.C. and B. Kivel. Physical Review 11. , v. 114, Slow electron scattering by atomic oxygen. 15 May 1959: 1026 - 1027. LowNeynaber, R.H., L.L. Marino, E.W. Rothe, and S.M. Trujillo. Physical Review energy electron scattering from atomic oxygen. v. 123, 1 July 1961: 148 - 152. , 12. Robinson, L.B. Elastic scattering of low-energy electrons by atomic Physical Review v. 105, 1 February nitrogen and atomic oxygen. , 1957: 922 - 927. 24- McGraw Hill, 1955. 13. Schiff, L.I. Quantum Mechanics 14. Scott, W.T. The Physics of Electricity and Magnetism and Sons, 1959. 15. Low-energy electron Sunshine, G., B.B. Aubrey, and B. Bederson. scattering by atomic oxygen. Proceedings of the Third International Conference on the Physics of Electronic and Atomic Collisions 1965 . . John Wiley , 130 16. - 133. Temkin, A. Polarization and exchange effects in the scattering of Physical Review electrons from atoms with application to oxygen. v. 107, 15 August 1957: 1004 - 1012. -25- , ( b/"[ jo srj-mn) £JT SU3 Q a8.iBti3 "[BfpB^ 26- 1 300 1 J 250 200 • 150 1 100 _i CM 0) >4-l o CO 4-1 •r-l c 3 S 50 V \ s. v • r v 4 S"~ (units of a o ) b -» BEHAVIOR OF THE CORE POTENTIAL, V„(r) H Figure 2 -27- |H A .8 • 1 • .6 • J, o w i 1 : fed U & C 3 \ ' \ 1\ f , i i. z r (units of a L^~™ -i ) POLARIZATION POTENTIAL WITH q = Figure 3 -28j- 5 A .8 [j .6 i \ CM ! ! 1 CO •1-1 C 3 1 .2 > T z> ! r (units of a ) ' i -* POLARIZATION POTENTIAL WITH q - Figure 4 -29- 8 ".- «_ v go S3T un ) uof303s sso.13 1*301 ( 6 30- » Vffi'' &3& lift a I: i H m m to z o H O l-l CO § «_ C % jo s^iun) UOT3D3S sscio "[«30i -31- vO 4) H 00 *o r 50 O <N .Hammerling,. et al *4-l o CO 40 Klein and Brueckner Energy (units of e /a Q ) THEORETICAL CROSS SECTIONS Figure 7 -32- 4<r O <M «d 4-1 O 30 Sunshine, et al o CO 4-1 •H d 3 £ O 2C a o CO CO o u i Neynaber, et al O cd o 10 X — Lin & Kivel rr TT Energy (units of e /a EXPERIMENTAL CROSS SECTIONS Figure 8 -33- 7*T ) ^ TABLE .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 1 ALPHA DELTAO DELTA1 DELTA2 DELTA3 9770 8872 8269 7813 7440 7122 6843 6594 6371 6167 1.5979 .5018 .5104 .5338 .5561 .5759 .5935 .6091 .6230 .6356 .6471 .6575 .0000 .0055 .0117 .0188 .0267 .0354 .0448 .0550 .0658 .0771 .0888 .0000 .0017 .0035 .0053 .0072 .0091 .0112 .0132 .0154 .0177 .0200 DELTAO DELTA1 DELTA2 DELFA3 9709 8719 8078 7598 7209 6878 6591 6335 6105 5897 5706 .5006 .5274 .5611 .5889 .6121 .6318 .6488 .6638 .6771 .6890 .6998 .0000 .0055 .0117 .0188 .0266 .0353 .0447 .0547 .0653 .0765 .0880 .0000 .0017 .0035 .0053 .0072 .0091 .0112 .0133 .0154 .0177 .0201 - .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 5.5 SIGMA 6678 7451 4121 5178 7739 5334 0109 3357 24.5858 24.8064 6 15 19 21 22 23 24 24 25.0224 SIGMA 10.4912 22.2733 27.5908 30.0143 30.9885 32.2318 31.1230 30.8598 30.5507 30.2516 29.9895 8 DELTAO DELTA1 DELTA2 DELTA3 9644 8554 7871 7366 6960 6617 6320 6057 5822 5610 5416 .5028 .5582 .6009 .6318 .6562 .6762 .6934 .7083 .7214 .7332 .7438 .0000 .0055 .0117 .0187 .0265 .0351 .0444 .0543 .0648 .0757 .0869 .0000 .0017 .0035 .0053 .0072 .0091 .0112 .0133 .0154 .0177 .0201 SIGMA 15 ,9588 36, ,8699 42 ,9553 43 ,8549 43, ,0616 41, .7041 40, ,2216 38, ,7979 37, ,5062 36, ,3703 35, 3891 ALL PHASE SHITT ANQbES AP6 QIV6N in MybTiPbes er pi RADIANS -34- TABLE 2 ALPHA = .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 = 6.0 5 DELI A0 DELTA1 DELTA2 DELTA3 9825 8977 8388 7939 7569 7253 6976 6729 6505 6301 6114 .5023 .5040 .5234 .5434 .5619 .5786 .5937 .6074 .6198 .6312 .6416 .0000 .0060 .0129 .0207 .0294 .0390 .0496 .0609 .0729 .0856 .0987 .0000 .0019 .0038 .0058 .0079 .0100 .0122 .0145 .0184 .0193 .0218 DELTAO DELTA1 DELTA2 DELTA3 9756 8810 8181 7707 7320 6992 9670 1.6450 1.6220 1.6012 1.5820 .5014 .5186 .5483 .5745 .5970 .6165 .6336 .6487 .6622 .6744 .6854 .0000 0060 .0128 .0206 .0293 .0389 .0493 .0605 .0724 .0848 .0976 .0000 .0019 .0038 .0058 .0079 .0100 .0122 .0145 .0168 .0193 .0219 DELTAO DELTA1 DELTA2 DELTA3 9685 8632 7959 7458 7054 6712 6415 6152 1.5917 1.5703 1.5509 .5006 .5426 .5830 .6140 .6390 .6599 .6778 .6934 .7072 .7196 .7307 .0000 .0060 .0128 .0206 .0292 .0387 .0490 .0600 .0717 .0838 .0963 .0000 .0019 .0038 .0058 .0079 .0100 .0122 .0145 .0168 .0193 .0219 SIGMA 4, ,0100 12, ,8560 16, ,3795 18, ,5432 20, ,0096 21, ,0657 21, ,8826 22, ,5658 23, ,1803 23 ,7635 24, ,3341 SIGMA • .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 . 7.4262 18.2930 23.2639 25.9655 27.4278 28.2089 28.6273 28.8643 29.0231 29.1604 29.3036 SIGMA 12, ,2868 28, ,7581 35, ,5747 37, ,9080 38, ,3704 38, ,0360 37, ,3904 36, ,6634 35, ,9643 35, ,3414 34, .8102 ALL PHASE SHIFT ANGLES ARE GIVEN IN MULTIPLES OF PI RADIANS -35- TABLE .0050 .0500 .1000 .1500 .2000 .2500 .3000 .3500 .4000 .4500 .5000 3 ALPHA = 0.0 DELT-AO DELTA1 DELTA2 DELTA3 1.9154 1.7502 6672 6121 5705 5370 5091 4850 4638 4450 4280 .5004 .5157 .5493 .6000 .6664 .7415 .8139 .8750 .9223 .9575 .9836 .0000 .0000 .0004 .0011 .0020 .0032 .0047 .0064 .0084 .0105 .0128 .0000 .0000 .0000 .0000 .0000 .0002 .0004 .0005 .0008 .0011 .0014 SIGMA 86.6421 63.6804 51.5073 48.9037 53.3931 60.4892 64.6529 63.9188 59.9304 54.7727 49.6356 ALL PHASE SHIFT ANGLES ARE GIVEN IN MULTIPLES OF PI RADIANS 1 -36- INITIAL DISTRIBUTION LIST No. Copies Defense Documentation Center Cameron Station Alexandria, Virginia 22314 20 Library U.S. Naval Postgraduate School, Monterey, California 2 Prof. William B. Zeleny Department of Physics US Naval Postgraduate School, Monterey, California 1 LT William L. Johnson Dept of Physics US Naval Postgraduate School, Monterey, California 1 . 37- Security Classification DOCUMENT CONTROL DATA (Security ctaaaitication ol ORIGINATING ACTIVITY 1. title, - R&D body ol abmtract and indexing annotation must be entered whan the overall report ie claaeiliad) 2a REPORT SECURITY C L ASSI Fl C A TION (Corporate author) Unclassified U.S. Naval Postgraduate School 26 CROUP REPORT TITLE 3. Elastic Scattering of Low-Energy Electrons from Oxygen 4. DESCRIPTIVE NOTES (Type 5. AUTHOR(S) ot report and incluaive dataa) N/A (Laat name, tint nemo, initial) Johnson, William L., LT, USNR REPORT DATE 6- 8a. 6. 27 May 1966 CONTRACT OR GRANT NO. PROJECT 7a. TOTAL 39 9a. ORIGINATOR'S REPORT NUMBERfSj 9b. OTHER REPORT NO. OF PAGES 7b. NO. OF REPS 16 NO. N/A N/A NOfSJ (Any othar numbara that mav be aaaitned thia report) N/A 10. Wi %i AVAILABILITY/LIMITATION NOTICES This document has been approved for publ: release and sale; its distribution is unl. 11. SUPPLEMENTARY NOTES 12- N/A 13. SPONSORING MILITARY ACTIVITY N/A ABSTRACT The cross sections for the elastic scattering of electrons from atomic and 13.6 electron volts. oxygen are calculated in the energy range between Polarization of the atom is included by using a term in the potential function which has the correct asymptotic behavior and which vanishes at the origin. Previous theoretical and experimental results are discussed. 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