Transport coefficients for NO+ ions in helium gas: a test of the NO+He interaction potential

Transport coefficients for NO+ ions in helium gas: a test of the NO+He interaction potential

Chemical Physics ELSEVIER Chemical Physics 211 (1996) 1-15 Transport coefficients for NO + ions in helium gas: a test of the NO +-He interaction pot...

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Chemical Physics ELSEVIER

Chemical Physics 211 (1996) 1-15

Transport coefficients for NO + ions in helium gas: a test of the NO +-He interaction potential Larry A. Viehland a,,, Alan S. Dickinson b, Robert G.A.R. Maclagan c a Parks College of Saint Louis University, Cahokia, Illinois 62206, USA b Department o f Physics, University o f Newcastle upon Tyne, Newcastle upon Tyne NEI 7RU, UK c Department of Chemistry, University o f Canterbury, Christchurch, New Zealand

Received 2 February 1996

Abstract

Transport cross-sections for the collision of positive nitrogen oxide ions with helium atoms have been computed from a theoretical NO +-He interaction potential. These cross-sections have been used in a kinetic theory of diatomic ion motion in atomic gases to determine the mobility and diffusion coefficients parallel and perpendicular to an external electric field. Comparison of the calculated mobilities with experimental data shows that theory and experiment agree within their mutual uncertainties.

1. Introduction

Helium is the buffer gas most often used in drift-tube studies of ion-neutral reaction rate coefficients, so understanding the transport coefficients of diatomic ions in helium and the ion velocity distribution functions is of considerable importance. Obtaining this understanding for NO + ions in He starts with knowledge of the ground-state potential energy surface over wide ranges of the N O + - H e separation, as a function of the angle between the N - O and N O + - H e axes. The only previous ab initio potential energy surfaces for the N O + - H e system are calculations of second order molecular properties using the time dependent coupled Hartree-Fock method by Visser and Wormer [1] and a recent CIPSI study by

Corresponding author.

Robbe et al. [2]; more accurate values are needed for the present purpose. From the interaction potential, the appropriate transport cross-sections may be calculated. Classical trajectory methods [3] have been shown recently [4] to give diffusion and viscosity cross-sections for the similar system, N f - H e , that are in agreement with quantal calculations within 2% for total energies above 2.3 X 10-4 hartree. They are therefore adopted here. The transport cross-sections may be used to compute the transport coefficients and ion velocity distribution function from equations obtained by solving the Boltzmann-like kinetic equation by a method of weighted residuals [5]. Vibrational excitation may be ignored, since recent calculations [6] for various initial rotational levels have shown the vibrational de-excitation cross-section from the v = 1 level of NO + to be below 0.005 square bohr for collision energies below 0.5 eV.

0301-0104/96/$15.00 Copyright © 1996 Elsevier Science B.V. All rights reserved. PH S0301 - 0 1 0 4 ( 9 6 ) 0 0 1 5 8 - 9

L.A. Viehland et al./Che m i c al Physics 211 (19961 1 15

Finally, comparison of the calculated transport coefficients with experimental values of the gaseous ion mobility [7,8] may be used to test the accuracy of the original interaction potential. Section 2 describes how points on the N O + - H e potential energy surface were obtained and used to determine the interaction potential at any separation and angle. Section 3 indicates how the classical trajectory calculations of the cross-sections were performed and their accuracy assessed. Calculated cross-sections, particularly the momentum-transfer cross-section, are discussed in Section 4. Technical details of how the kinetic theory was used to calculate the gaseous ion transport coefficients from the cross-sections are given in Section 5. Section 6 contains a comparison of calculated and measured mobilities for NO + ions in He gas. Conclusions are given in Section 7.

2. Potential energy surface A semiempirical potential energy surface for the N O ÷ - H e interaction has been described by Zenevich et al. [9] and used to calculate rate constants for vibrational relaxation. This work drew on the earlier work of Gislason and Ferguson [10], which predicted a well depth for the interaction of 2.1 × 10- 3 hartree. The CIPSI study [2], in which the N - O bond length was kepot fixed at its experimental value [11] of 1.0632 A, found a minimum in the potential energy surface with a depth of 1.1 × 10 -3 hartree located 2.96 A from the center of mass of the NO fragment and at an angle of 70.1 ° on the side of the oxygen atom. Calculations on the Li+-N2 and L i + - C O systems by Grice et al. [12,13] demonstrated that the M P 4 S D T Q / 6 - 3 1 1 + G(2df, p) level of theory gave values of structural and thermodynamic properties in close agreement with experiment. In particular, the transport properties calculated using these potentials were in good agreement with experiment. This is a higher level of theory than was used in the CIPSI study. Therefore, in this work we have performed new ab initio calculations of the N O + - H e potential energy surface using the G A U S S I A N 92 program [14] at the M P 4 S D T Q / 6 - 3 1 1 + G(2df, p) level. The NO + bond length in these calculations was fixed at

1.0262 A, the optimum bond length obtained from a H F / 6 - 3 1 1 + G(2df,p) optimization. The origin of the coordinate system was the center of the N - O bond and the polar angle, 0, was measured from the nitrogen atom. The values we have calculated for the ground state N O + - H e potential energy surface are given in Table 1. These values cover 42 ion-atom separations, r, from 1.4 to 18.0 ,~ (measured from the NO + midpoint) at each of 9 polar angles, 0, separated by "rr/8 in the range [0,v]. The values are given to more digits than we believe are accurate only because these are the values actually used in the calculations reported below. The potential energy at infinite separation between NO + and He is estimated to be - 132.2663702 hartree. The potential we have calculated has a single minimum with a depth of 6 . 6 4 9 × 10 ~ hartree at r = 2 . 9 0 ,~ and 0 = 100 °. Note that the depth is significantly smaller and at a significantly different angle than in the previous calculations discussed above. Since our potential energy surface was calculated, a CCSD(T) calculation has appeared [6]. This calculation used an augmented correlation-consistent quadruple-zeta basis set to which was added the df functions from the augmented, correlation-consistent triple zeta-basis set. It led to a well depth of 8.49 × 10 -4 hartree at r = 2.80 ,~ and 0 = 100.2 °, where r and 0 are determined with respect to the center of mass of the NO bond. In order to interpolate among the energies in Table 1, we assume that they can be represented by an expansion in Legendre polynomials, 8

V(r,O) = ~, Pi(cosO)Vi(r ).

(1)

i-O

This means that the tabulated values must satisfy the equation 8

V(r;,Oj)= ~,,MidVi(r,)

0_
1 _
i=0

(2) where the coefficients are

Mi,j=Pi(cosOj)

0_
1_
(3)

The square matrix M was inverted numerically, giving numerical values for the inverse matrix M L.

L.A. Viehland et a l . / Chemical Physics 211 (1996) 1-15

Therefore, at each angle 0 i we obtained numerical values of Vi(r) at the 42 ion-atom separations represented by r~, by using the equation:

8

Vi(r,)= Y'.M].,'V(r,,Oj)

0
1<1<42.

j 0

(4) We used the values at the two smallest separations to obtain the quantities and in the functional form

A(O)

V( r,O) = A( O)r-'(°)

n(O)

(5)

Then we generated another point at a separation of 0.7 A. from this functional form. Finally, we performed a spline fit at each value of i to the 43 points listed in Table 2, with the spline constrained to match the ion-induced dipole functional form:

V(r,O) =

-Car

-4,

(6)

at large separations. The quantity C 4 is determined o by the points at a separation of 18.0 A, where the potential is isotropic. Constraining the spline in this way was necessary because at separations greater o than about 10 A, the calculated energies appear not to be accurate enough to give the correct r-4 dependence.

3. Classical trajectories The classical trajectory program used to calculate the cross-sections from the interaction potential was based on earlier programs for neutral diatom-atom collisions [15] and for atomic ion-diatom collisions [3]. It was, however, extensively revised to compute the type of cross-section discussed below and to provide for automatic changes in the tolerance parameter governing the accuracy of a trajectory. A copy of this Fortran 90 program can be obtained by e-mail from [email protected]. The classical trajectory program assumes that the ion-neutral separation is measured from the centerof-mass of the diatomic ion, whereas the potential described in Section 2 was determined for separations measured from the midpoint of the N - O bond. Since we are interested only in low energy collisions that do not probe small separations, this small differ-

3

ence is not significant and in the interests of computing time we did not make use of a subroutine to convert from one coordinate system to the other. The transport cross-sections of interest are defined by [5]

O ',v '," A

e,< ) 1

=2rrfo~dbb(1)fl dcosx(2---~) r2rr X J0

[ l

[

d&,.[~-w)f02"~dqSj

k

X'(l',q'[l,q)~°,

E~] X'(l"q'll'q)k] ~"

(7)

Here E and E' are the pre- and post-collision values of the relative kinetic energy, E r and E'r are the pre- and post-collision values of the internal (rotational) energy of the ion, b is the impact parameter, X is the angle between the pre-collision rotational angular momentum ( j ) of the diatomic ion and the pre-collision orbital angular momentum (L) of the relative motion, 4,t is the angle conjugate to L, and q5a is the angle conjugate to j. The relationship between these variables, r and 0 is given by Smith [16] in action-angle variables. The use of action-angle variables facilitates the calculation of the cross-sections from the interaction potential by classical trajectory methods. The transport cross-sections are normalized to be equal to q-rd2 for rigid spheres of diameter d bohr. They involve the complex conjugate (represented by * ) of differences between detailed opacity functions before and after collisions. They are characterized by the seven indices in the subscript and superscript. The A and B indices refer to powers of the ratios of the pre- and post-collision values of E and Er, respectively. The l and l' indices label the tensorial character of the opacity functions in velocity space, while the q and q' indices similarly label the opacities in angular momentum space. The k index labels the overall tensorial character of the basis functions, subject to the requirement that the cross-sections vanish unless

Iq-q'l
(8)

L.A. Viehland et a L / C h e m i c a l Physics 211 (1996) l 15

4

The detailed expression for the opacity functions

where the components of the spherical tensors of rank k are defined in terms of spherical harmonics

is: [17]

asz

x ' ( ' l ,q ' II,q),.

Y( l,l',k,m;5,,5/) =(-1)"(2k+

(21'+l)'/2(2q'+l)'/2(2k+ ×

1) ,

q,q

("'

,k,m; j,j ),

1

interaction

potential

V,(r,O),

in atomic

units,

r

0 = 0°

0=

1.40000000

-

131.6181659

-

1.50000000

-

131.7280375

1.62500000

-

131.9155829

-

1.75000000

-

132.0427903

1.87500000

-

132.1263110

for NO

22.5 °

~

He 0 = 67.5 °

0=

131.8531873

-

132.0581981

-

132.1379836

-132.1452299

131.9399998

-

132.1099095

-

132.1763952

-

132.0369112

-

132.1603361

-

132.2099643

-

132.1131402

-

132.1969023

-

132.2319215

-

132.2376731

-

132.1677462

-

132.2222696

-

132.2459484

-

132.2500198

0=

45 °

90 °

132.1848058 132.2174481

2.00000000

-

132.1799773

-

132.2046225

-

132.2392144

-

132.2547063

-132.2574324

2.12500000

-

132.2138982

-

132.2286146

-

132.2501776

-

132.2600486

-

132.2617950

2.18750000

-

132.2257274

-

132.2371020

-

132.2540371

-

132.2618481

-

132.2632253

2.25000000

-

132.2350295

-132.2438196

-

132.2570785

-132.2632252

-

132.2643017

2.31250000

-

132.2423206

-

-

132.2594605

-

132.2642705

-

132.2651055

132.2491111

(10)

In Eq. (7) the superscript on the opacity function means that the primed (post-collision) velocity and

(9)

The

_km)Y,'(})Y,~,'(}' ) .

p

m

Table

1) I/2

2.37500000

-

132.2480176

-

132.2532608

-

132.2613142

-

132.2650567

-

132.2657001

2.43750000

-

132.2524559

-

132.2565012

-

132.2627471

-

132.2656417

-

132.2661353

2.50000000

-

132.2559035

-

132.2590206

-

132.2638467

-

132.2660718

2.56250000

-

132.2585730

-

132.2609702

-

132.2646837

-

132.2663834

-

2.62500000

-

132.2606327

-

132.2624710

-

132.2653153

-

132.2666051

-132.2668244

2.68750000

-

132.2622151

-

132.2636197

-

132.2657871

-

132.2667591

-

2.75000000

-

132.2634250

-

132.2644931

-

132.2661355

-

132.2668625

-

132.2669878

2.81250000

-

132.2643445

-

132.2651522

-132.2663893

-

132.2669283

-

132.2670214

132.2664492 132.2666714

132.2669255

2.87500000

-

132.2650388

-

132.2656455

-

132.2665710

-

132.2669665

-

132.2670340

2.93750000

-

132.2655590

-

132.2660111

-

132.2666983

-

132.2669845

-

132.2670312

3.00000000

-

132.2659452

-

132.2662791

-

132.2667845

-

132.2669877

-132.2670177

3.12500000

-

132.2664353

-

132.2666105

-

132.2668732

-

132.2669657

-132.2669708

3.25000000

-

132.2666853

-

132.2667696

-

132.2668934

-

132.2669228

-132.2669115

3.50000000

-

132.2668378

-

132.2668415

-

132.2668426

-

132.2668184

-

132.2667909

3.62500000

-

132.2668341

-

132.2668222

-

132.2668002

-

132.2667675

-

132.2667369

3.75000000

-

132.2668083

-

132.2667889

-132.2667561

-

132.2667205

3.87500000

-

132.2667719

-

132.2667497

-

132.2667133

-

132.2666779

-

132.2666463

4.00000000

-

132.2667317

-

132.2667094

-

132.2666734

-

132.2666398

-

132.2666090

4.25000000

-

132.2666539

-

132.2666349

-

132.2666042

-

132.2665755

-

132.2665479

4.50000000

-

132.2665861

-

132.2665719

-

132.2665482

-

132.2665248

-

132.2665017

4.75000000

-

132.2665317

-

132.2665213

132.2664849

-

132.2664669

5.00000000

-

132.2664894

-

132.2664818

-132.2664680

-

132.2664543

5.50000000

-

132.2664324

-

132.2664285

-

132.2664213

-

132.2664150

-

132.2664096

6.00000000

-

132.2664027

132.2664010

-

132.2663981

-

132.2663957

-

132.2663939

7.00000000

-

132.2663793

132.2663794

-

132.2663796

-

132.2663798

-

8.00000000

-

132.2663771

-

132.2663771

-132.2663770

-

132.2663769

132.2663769

9.00000000

-

132.2663755

-

132.2663755

-

132.2663752

-

132.2663750

132.2663748

10.00000000

-

132.2663731

-

132.2663731

-

132.2663731

-

132.2663731

12.00000000

-

132.2663717

-

132.2663717

-

132.2663717

-

132.2663717

-

132.2665032

132.2663711

132.2666888

132.2664413

132.2663802

132.2663730 -

132.2663717 132.2663711

14.00000000

-

132.2663711

132.2663711

-

132.2663711

-

16.00000000

-

132.2663709

132.2663709

-

132.2663709

-

132.2663709

-132.2663709

18.00000000

-

132.2663707

132.2663707

-

132.2663707

-

132.2663707

132.2663707

L.A. Viehland et al. / Chemical Physics 21l (1996~ 1-15

5

Table 1 (continued) r

0=

112.5 °

0 =

135 °

1.40000000

-

132.1115365

-

132.0114948

1.50000000

-

132.1606440

-

132.0844383

1.62500000

-

132.2019377

1.75000000

-

132.2279662

-

132.1944673

1.87500000

-

132.2440761

-

132.2229637

2.00000000

-132.2538609

0 =

157.5 °

0 =

180 °

131.7967297

-

131.9199090

-

I31.7513731

132.0402778

-

131.9468738

-

132.1244385

-

132.0713694

-

132.1796957

-

-

132.1503774

132.2408825

132.2146441

131.5230383

132.1490622 132,1968400

2.12500000

-132.2596834

-

132.2518794

-

132.2362059

2.18750000

-

-

132.2556050

-

132.2435571

-

2.25000000

-132.2630714

-132.2584714

132.2492453

-

132.2432502

2.31250000

-

132.2641719

-

132.2606637

-

132.2536261

-

132.2490790

2.37500000

-

132.2649956

-

132.2623304

-

132.2569840

-

I32.2535461

2.43750000

-

132.2656075

-

132.2635898

-

132.2595454

-

132.2569563

2.50000000

-

132.2660582

-

132.2645358

-

132.2614893

-

132.2595488

2.56250000

-

132.2663861

-

132.2652417

-

132.2629570

-

132.2615106

2.62500000

-

132.2666209

-

132.2657649

-

132.2640593

-

132.2629878

2.68750000

-

132.2667850

132.2661492

-

132.2648822

-

132.2640941

2.75000000

-

132.2668956

-

132.2664282

-

132.2654926

-

132.2649176

2.81250000

-

132.2669656

-

132.2666276

-

132.2659418

-

132.2655262

2.87500000

-

132.2670051

-

132.2667665

-

132.2662691

-

132.2659723

2.93750000

-

132.2670220

-

132.2668597

132.2665044

-

132.2662957

3.00000000

-

132.2670222

-

132.2669183

-

132.2666702

-

132.2665267

3.12500000

-

132.2669902

-

132.2669640

-

132.2668576

-

132.2667977

3.25000000

-

132.2669353

-

132.2669513

-

I32.2669244

-

132.2669094

3.50000000

-

132.2668101

132.2668543

-

132.2668909

-

132.2669107

3.62500000

-

132.2667517

-

132.2667968

-

132.2668418

-

132.2668661

3.75000000

-

132.2666993

-

132.2667417

-

132,2667880

-

132.2668130

3.87500000

-

132.2666530

-

132.2666911

-

132.2667353

-

132.2667590

4.00000000

-

132.2666125

-

132.2666459

-

132,2666862

-

132.2667077

4.25000000

-132.2665467

-

132.2665713

-

132.2666026

-

132.2666189

4.50000000

-

132.2664980

132.2665152

-

132.2665378

-

132.2665491

4.75000000

-

132.2664624

-

132.2664737

-

132.2664893

-

132.2664968

5.00000000

-

132.2664371

-

132.2664440

-

132.2664543

-

132.2664592

132.2664073

-

132.2664094

-

132.2664131

-

132.2664149

132.2663931

-132.2663937

-

132.2663948

-

132.2663953

-

132.2663802

-

132.2663800

-

132.2663798 132.2663770

5.50000000

132.2616105

132,2258521 132.2356718

6.00000000

-

7.00000000

-132.2663804

8.00000000

-

132.2663769

132.2663769

-

132.2663770

-

9.00000000

-

132.2663747

-

132.2663748

-

132.2663750

-

132.2663751

10.00000000

-

132.2663730

-

132.2663731

-

132.2663731

-

132.2663731

-

132.2663717

-

132.2663717

132.266371l

-

132.2663711

12.00000000

-

132.2663717

-

132.2663717

14.00000000

-

132.26663711

-

132.2663711

t6.00000000

-

132.2663709

-

132.2663709

-

132.2663709

-

132.2663709

18.00000000

-

132.2663707

-

132.2663707

-

132.2663707

-

132.2663707

angular momentum in Eqs. (9) and (10) are replaced by the unprimed (pre-collision) quantities. The equations above imply that the detailed opacity functions are proportional to scalar products of spherical tensors of the same rank, and hence that they are invariant to a simultaneous rotation of all four unit vectors ( ~ , ~ , ' , ] and f , the pre- and postcollision angles associated with the relative velocity

v between the ion and atom and with j ) by a single rotation. Since the relative velocity is a true vector, with v going to - v when reflected through the origin, this leads to a parity restriction: the transport cross-sections vanish when l + l' is odd. However, j is a pseudo-vector, remaining unchanged when reflected through the origin. This means that the cross-sections are real if q + q' is even, and imagi-

6.2747 0.2153 0.1563 0.1011 6.3473E-02 3.8757E-02 2.3018E-02 1.3243E-02 9.8980E-03 7.3066E-03 5.3101E-03 3.7807E-03 2.6160E-03 1.7349E-03 1.0734E-03 5.8107E-04 2.1858E-04 - 4.4640E-05 - 2.3227E-04 - 3.6263E-04

3.4173 - 3.3035E - 02 - 1.4333E-02 - 3.1903E-03 1.4271E-03 2.7800E-03 2.7509E-03 2.2513E-03 1.9600E-03 1.6760E-03 1.4118E-03 1.1745E-03 9.6661E-04 7.8840E-04 6.3844E-04 5.1442E-04 4.1323E-04 3.3167E-04 2.6649E 04 2.1453E-04

i=1 1.3017 0.2570 0.2034 0.1407 9.2948E-02 5.9493E-02 3.7230E-02 2.2876E-02 1.7822E-02 1.3830E-02 1.0691E-02 8.2317E-03 6.3126E-03 4.8201E-03 3.6635E-03 2.7700E-03 2.0817E-03 1.5531E-03 1.1481E-03 8.3871E-04

i=2 1.0878 2.1073E-04 8.5149E-03 8.9646E-03 7.6044E-03 5.7694E-03 4.1233E-03 2.8488E-03 2.3487E-03 1.9280E-03 1.5758E-03 1.2816E-03 1.0360E-03 8.3111E-04 6.6099E-04 5.2069E-04 4.0615E-04 3.1388E-04 2.4077E-04 1.8390E-04

i=3 3.1492 0.1206 9.3998E-02 6.0771E-02 3.7971E-02 2.3283E-02 1.4133E-02 8.5224E-03 6.6034E-03 5.1086E-03 3.9455E-03 3.0414E 03 2.3391E-03 1.7944E-03 1.3725E-03 1.0469E-03 7.9635E-04 6.0428E 04 4.5770E-04 3.4605E-04

i=4

2.6553 - 3.8148E-03 6.5981E-03 4.7601E-03 3.0841E-03 1.9054E-03 1.1540E-03 6.9386E-04 5.3929E-04 4.2201E-04 3.3401E-04 2.6853E-04 2.1974E-04 1.8265E-04 1.5340E-04 1.2930E-04 1.0864E 04 9.0496E-05 7.4285E 05 5.9909E-05

i=5

3.5115 6.6642E-02 4.8149E-02 2.3063E-02 1.1288E-02 5.7101E-03 2.9773E-03 1.5911E-03 1.1720E-03 8.6708E-04 6.4426E-04 4.8028E-04 3.5907E-04 2.6848E-04 2.0040E-04 1.4879E-04 1.0951E 04 7.9465E-05 5.6753E 05 3.9614E-05

i=6

in atomic units (bohr and hartree) for the expansion of the potential energy surface in Legendre polynomials

0.7000 1.4000 1.5000 1.6250 1.7500 1.8750 2.0000 2.1250 2.1875 2.2500 2.3125 2.3750 2.4375 2.5000 2.5625 2.6250 2.6875 2.7500 2.8125 2.8750

V,(r),

i=0

r

Table 2 Coefficients

- 5.5830 - 1.0925E-02 1.0888E-02 5.1110E-03 2.1740E-03 9.2077E-04 4.0318E-04 1.8297E-04 1.2416E-04 8.4404E-05 5.7530E-05 3.9627E-05 2.7863E-05 2.0492E-05 1.5974E-05 1.3141E-05 1.1478E-05 1.0255E-05 9.2996E-06 8.4059E-06

i=7

2.6950 3.6254E-02 2.4853E-02 9.4526E-03 3.6103E 03 1.4407E-03 6.0337E-04 2.6268E-04 1.7527E-04 1.1777E-04 7.9597E-05 5.4279E-05 3.7395E-05 2.6113E-05 1.8491E-05 1.3192E-05 9.4205E-06 6.6834E-06 4.5352E-06 2.9121E-06

i=8

C3~

Ixa

.-z.

e~

5~

4.0789E-04

1

E

-

0

4

1

1

5

8

E

-

0

4

9.8319E-06

2.5105E-05

4.3428E-05

8.1233E-05

-

0

0

E

-

0

6

-5.1658E-07

0

- 7.0000E-07

5

16.000

.

18.000

1

2.8622E-06

9.0000E-07

-

-

14.000

12.000

I0.000

4.8027E-06

.

4

9.0000

1

5

1.5221E-04

0

- 6.7383E-06

-

-

-

-

-

-

.

8.0000

7.0000

6.0000

5.5000

5.0000

4.7500

4.5000

2

- 2.7389E-04

4.0000

-

- 3.1463E-04

3.8750

4.2500

3.5953E-04

3.7500

-

- 4.5756E-04

3.6250

5.3944E-04

3.5000

-

5.4836E-04

3.2500

-

4.4982E-04

3.1250

-

5.0462E-04

2.9375

3.0000

1

.

9

8

7

E

-

0

5

2.3092E-05

1.9090E-05

4

8.6621E-06

1.6974E 05

2.0752E-05

2.0764E-08

2.8248E-07

5.2275E-08

- 2.4815E-23

- 7.2792E-23

1.9852E-23

- 4.1690E-22

-

-

-

4.5259E-07

- 3.2761E-06

-

-

-

- 2.3134E-05

-

8.7392E-06

4.3573E-07

1.3489E-05

5.6455E-05

9.0691E-05

1.3990E-04

1.7311E-04

6.0278E-04

4

.

1

1

1

1

E

-

0

5

5.4704E-05

6.8438E-05

7.4175E-05

7.6812E-05

1.9852E-23

6.6174E-23

7.4556E*08

- 3.3891E-07

- 2.6470E-23

- 6.6174E-24

-

-1.1472E-07

3.7422E-07

- 3.1321E-06

8.7269E-06

- 2.0783E-05

- 2.9767E-05

-

-

-

-

-

7.3230E-05

- 5.7837E-05

5 . 0 9 5 9 E 05

1.8503E-04

4.2347E-04

8.1348E-08

6.9926E-07

-

1.0588E-22

1.8529E-22

- 3.1764E-22

4.8969E-22

5.5321E-08

7.4911E-08

- 1.8527E-08

- 2.2777E-07

-

3.6766E-06

5.9506E-06

8.1502E-06

9.8557E-06

1.1468E-05

1.2501E-05

1.4138E-05

1.6882E-05

2.1416E-05

4.2022E-05

6.5115E-05

1.0755E-04

1.4040E-04

1.5805E-06

2.2594E-06

5.3018E-08

2.9845E-08

3.9948E-08

5.6465E-08

4.6219E-07

- 1.9852E-23

1.3235E-23

- 6.6174E-23

- 2.9117E-22

-

-

- 1.0637E-06

-1.2953E-06

- 1.2837E-06

-

-1.9571E-06

- 7.9175E-07

1.9472E 06

7.3244E-06

1.7015E-05

6.2620E-05

1.1192E-04

1.9731E-04

2.6150E-04

4.6389E-06

2.5546E-06

-

2.8969E-08 5.7394E-08

- 9.2644E-23

-- 2 . 6 4 7 0 E - 2 3

6.6174E-23

- 5.2940E-23

-

3.7704E-08

8.0203E-08

2.8986E-07

- 7.9303E-07

- 1.7536E-06

-

- 3.4722E-06

- 4.3157E-06

-

4.4215E-06

- 3.7121E-06

- 2.2550E-06

1.9672E-07

1.0475E-05

2.0775E-05

3.6833E-05

4.7455E-05

8 . 3 0 9 2 E 07

5.2678E-06

5.6376E-06

5.8829E-06

5.8447E-06

3.8488E-06 1.4090E 0 6

2.3994E-09

2.7040E-08

2.3698E-08

6.8480E-08

2.1583E-07

3 . 9 7 0 5 E 23

7.9409E-23

1.5882E-22

0.000

-1.6230E-08

-

-7.5673E-07

-

-2.4376E-06

-

-5.1781E-06

-

-

- 5.3056E-06

-

1.7210E-05

2.6653E-05

/.3850E-06

-

-

1.3235E-22

1.5882E 22

2.1176E-22

3.1764E-22

2.2836E-08

1.6534E-08

1.6901 E-08

8.0026E-08

5.2656E-08

5.869E-09

4.8766E-08

6.8938E-08

- 4 . 4 3 4 7 E 08

3.7282E-08

2.6007E-07

4.4167E-07

6.6360E-07

9.3748E-07

1.3485E-06

3.0979E-06

4.6181E-06

6.4621E-06

1.7345E*06

5 . 8 8 7 8 E 08 3.1826E-08 3.1826E-08

[ .0588E-22

- 2.6470E-23

5.2940E-23

- 1.0588E-22

-

- 2.6470E-22

1.9096E-08

1.5913E-08

- 1.7504E-08

-

- 1.5913E-08

-

2.0687E-08

3.1826E-08

9.3887E-08

- 6.3652E-08

-

- 1.7504E-07

- 2.6416E-07

- 3.6600E-07

- 4.6148E-07

- 1 . 5 9 1 3 E 07

8.7521E-07

t,~

3"

8

L.A. Viehland et al. / Chemical Physics 211 (19961 1 15

nary if the sum is odd. Of course, the real and imaginary cross-sections couple with the real and imaginary expansion coefficients (see Section 5) in such manner that only real values are obtained for the transport coefficients and distribution function. This does not mean, however, that we can skip the calculation of the imaginary cross-sections, which at one point we did inadvertently by restricting the range of 4,/ to [0,'rr] rather than using the full range

400

'1 300~

[0,2~]. In order to obtain accurate cross-sections, it is important to sample enough values of the four integration variables in Eq. (7). We repeatedly recalculated the m o m e n t u m - t r a n s f e r cross-section 0~°'°'l'~'l'°)(E,E~), hereafter designated as Qm, at high values of E and E~ using different numbers of these variables. We established that Qm is accurate within a few tenths of a percent when we sample ten impact parameters below 7.0 bohr, three larger impact parameters with the value of C [3] chosen as 0.30, and ten values for each of the three angular variables. At values of E below 0.001 hartree, we increased both the division point and the value of C, depending on E, to ensure that the contribution of the long-range tail was included. As a check, eleven cross-sections were compared with values calculated using the independent atom-molecule code [15].

Q,n

200

~

~il

~x 1

0

......

0

~

T~7~27"27 . . . . .

~

a

± a ± ~ z ±

a

~

a

*IZiIZZ

0

I

a

'

a

I

0.0001

a a a ±

0.001

I

I

0.01

0.t

I

1

,

.__ i

10

Er Fig. 1. The momentum-transfer cross-section, Qm, as a function of the rotational energy, Er, in atomic units. The delta symbols indicate the computed values, while the straight lines connecting the symbols are used only as a guide for the eye. From top to bottom, the curves correspond to E values of 0.0001000, 0.0001778, 0.0003162, 0.0005623, 0.0010000, 0.0017780, 0.0031620, 0.0056230 and 0.0100000 a.u.

4. Cross-sections

The cross-sections defined by Eq. (7) have been computed using the techniques described in Section 3. Fig. 1 shows how the most important cross-section, that for momentum-transfer, Qm, varies with E r at low E. The accuracy of Qm when both E and Er are low is clearly not very high, indicating that even more trajectories should have been sampled in this situation. However, such inaccuracies should have no importance for the calculations reported in Section 5, since the presence of an electric field will cause the average collision energy to increase from the thermal energy at 300 K, 9.5 × 10 -4 hartree. The strong dependence on E~ shown for E = 0.0001 hartree is primarily associated with the (E'/E) 1/2 factor appearing in the integral, 1 ( E ' / E ) ~/2 cos 0. Simply integrating 1 - c o s 0 for

the 3 cases E r = 0 . 0 0 0 1 , 0.001 and 0.01 hartree gives cross-sections varying by about 10%. Note from Fig. 1 that at E = 0.0005623 hartree, the cross-section shows two peaks, one near Er = 0.001 hartree and a second, larger peak near 0.02 hartree. The small peak shifts to smaller E r and disappears as E decreases, but the large peak remains near 0.02 hartree for all E values below about 0.0025 hartree. Above E = 0.010 hartree there appears to be only one peak, which gradually shifts to higher E r for E > 0.0025 hartree and diminishes in amplitude as E increases. One way to understand the transition from low to high E r behavior is to look at the adiabaticity parameter,

z-

w Ro( b,v) V

(ll)

L.A. Viehland et ell. / Chemical Physics 211 (1996) l - 15

9

Table 3 Indices for tile cross-sections calculated in this work. Each group of seven integers consists of the values of q,q',l,l', A,B, and k in Eq. (7) 0(~0010 0011310 0122201 1011301 1111101 1111311 1211102 2(502222 2(520022 2(131122 2111111 2120212 2211102 2240004

0000020 0011320 0122211 1011311 lllll02 1111312 1211301 2011102 2020202 2031302 2111112 2131102 2211300

0000200 0022200 0211102 1022201 1111110 1120002 1211302 2011112 2020212 2031312 2111301 2131103 2211301

0000210 0022210 0211302 1022211 Illllll 1120012 1220002 2011122 2020222 2031322 2111302 2131112 2211302

0000220 0022220 0220002 1100000 1111112 1120202 1220202 2011302 2022202 2042202 2111311 2131113 2220002

Here w is the rotor angular speed and R 0 is distance of closest approach, which depends upon the impact parameter, b, and the initial speed of relative motion, v. Crudely speaking, small z gives sudden collisions, where the trajectories at different initial orientations sample the full potential, and large z gives adiabatic collisions, where they sample the angle-averaged potential. For each (E, E~) pair, what matters is where the boundary z = 1 comes for the largest contributing impact parameter. We have looked in detail at the case where E = 0.008 hartree. Here the largest contributing impact parameter is b = 6 bohr, and z = 1 when E ~ = 0.002 hartree. We expect, therefore, that the collisions will be sudden, independent of E r up to about this value, which is consistent with Fig. 1. As E r increases further, the boundary between sudden and adiabatic collisions moves to smaller impact parameters, so the cross-section will continue to vary with E r until an E r value is reached above which effectively all collisions, even the clos-

0011100 0111101 0220202 ll00010 1111300 1120212 1231102 2011312 2022212 2042212 2111312 2200000 2220202

0011110 0111111 0231102 1100200 llll301 1131102 1231103 2011322 2022222 2042222 2120002 2200200 2231102

0011120 0111301 10Il l 01 1100210 1111302 1131112 2002202 2020002 2031102 2111101 2120012 2211100 2231103

0011300 0111311 1011111 1111100 1111310 1211101 2002212 2020012 2031112 2111102 2120202 2211101 2231104

est, are adiabatic. This pattern is displayed also at higher E values, although the structure is getting less marked as E increases. At very low E, less than 0.001 hartree or about two times the typical well depth, we get extra structure in the plot of Q,11 as a function of E r. This may be because the collisions at small impact parameters have a glory minimum, followed by a rainbow maximum at larger b. It is also possible that the extra structure occurs because the relation between the averaged potential and the full potential is different for the attractive and repulsive portions of the potential. Our calculations do not allow us to distinguish between these possibilities. Table 3 contains a list of the 118 cross-sections that we have calculated at 33 Er values (8 per decade between 10 -4 and 0.1 hartree and 4 per decade between 0.1 and 10 hartree), using 21 E values (4 per decade between 10 -4 and 1.0 hartree) for each E r. These are most of the cross-sections

Table 4 Indices for the cross-sections assumed to be negligible in this work. Each group of seven integers consists of the values of q,q',l,l', A,B, and k in Eq. (7) 0000400 1011321 1122201 1202202 2020422 2122212 2222200

0000410 1022221 1122202 1220402 2102202 2122213 2222201

0000420 1100400 1122210 1222201 2102212 2131302 2222202

0202202 1100410 1122211 1222202 2120402 2131312 2222203

0220402 1102202 1122212 1222203 2120412 2142202 2222204

0222202 1102212 1131302 1231302 2122201 2142212 2231302

0231302 1120402 1131312 1242202 2122202 2200400 2242202

0242202 1120412 1142202 2020402 2122203 2202202

1011121 1122200 1142212 2020412 2122211 2220402

10

L.A. V i e h l a n d et a l. / C h e m i c a l P h y s i c s 211 (1996) 1 - 15

needed to calculate the first two approximations ( N = 2) to the transport coefficients according to the scheme proposed earlier [5]:

i

0 < k< min(2N,/%), 0_


max(k,p),Sm) ,

0_< t < m i n ( N -

max(k,q),t

m).

i

I

O
i

o~L_

(12)

Those not calculated, and therefore assumed to be negligibly small, are listed in Table 4. It should be noted that the number of cross-sections required according to the scheme in Eq. (12) grows very rapidly, from 179 for N = 2 to 1056 for N = 3, which is why we have chosen to limit our considerations to no higher than second approximation of the kinetic theory. This second approximation is equivalent to the second approximation in the kinetic theory of transport for neutral atoms in that the crosssections we have retained correspond to retaining only the familiar Q(I}(E) and Q(2)(E) cross-sections of that theory. Cross-sections of the type 0(o°"°"°°"°"8)( E, E r) with B > 0 illustrate another difficulty. These cross-sections have as integrands in Eq. (7) the quantity I-(E'F/E~) 8. When E~ is much larger than E, collisions are nearly adiabatic and will generally result in a relatively small loss of internal energy, so cross-sections of this type vanish. When E r is much less than E, collisions will generally be superelastic (E'~ > > E r) and the cross-sections become large and negative. The behavior at small E~ can be factored out by always considering the product Eft O,~°°°'°'°'B)(E,E~), as shown in Fig. 2. Note from this figure that unusual behavior occurs at energies near 0.02 hartree, just as it did in Fig. 1. Unusual behavior at 0,02 hartree is a general feature of all the transport cross-sections we have examined, and we presume it results from the factors already discussed. In order to compute gaseous ion transport coefficients and ion velocity distribution functions, the transport cross-sections must be integrated over both E and E~. Eq. (C.39) of our previous work [5] shows that these integrands always involve products of the transport cross-sections and both powers and exponentials of E,.. After some numerical experimentation, we found that satisfactory values for the inte-

ErO

"0.()001

0.001

OOl

0.1

1

10

E, Fig. 2. The product of the transport cross-section Q~o°'°'°'°'°'l)( E,E r)

and the rotational energy E~, as a function of Er, in atomic units. The symbols and curves are as in Fig. 1.

grated cross-sections could be obtained if instead of spline fits of the cross-sections we used a two-dimensional ( E and E~) spline fit of the quantities:

Er

B+(q+q')/2

(~3) Note that the coefficients for the spline fit must be recomputed at each new value of the ion temperature, Tj, but this takes negligible computer time compared to the other parts of the calculations described in Section 5. The highest ion temperature needed to compare with experimental mobilities is about 4000 K [8]. The exponential term in Eq. (13) makes the crosssections at energies above about ten times kT~ (i.e., above 0.1 hartree) unimportant. We have calculated cross-sections at higher E and E r values in order to facilitate numerical integrations over these energies,

L.A. Viehland et al. / Chemical Physics 211 (1996) 1-15

but errors introduced by extrapolating into energy regions where the potential has not been computed (see Section 2) are negligible due to the exponential damping in Eq. (13). For the low E,, sudden collisions, the O,~ values are reasonably approximated by the limiting value for the polarization potential, Eq. (6). When E is in hartree, we have: [18] lira Qm

g~0

The trial and weighting functions we use are modeled after the basis functions of Curtiss [21] but modified in the manner of Kumar [22,23] so as to allow the ions to have kinetic and internal temperatures different from the gas temperature, and in the manner of Ness and Viehland [24] to take into account the use of two ion kinetic temperatures. They are given by the equation

B(k,m;p,q,s,tlvj)

(5'8b°hr2) E-I/2

=

I1

At the smallest E value considered, 0.0001 hartree, the sudden limit is never reached since E r > E for all & , as discussed with regard to Eq. (11).

= ( - I) ~-'(4k

+ 2)'/2WP-L(('+ p

q

T)(W 2) .,,/2

k

,u.v

15) 5. K i n e t i c

where

theory

We are interested in the transport coefficients and ion distribution function describing the steady-state motion of trace amounts of NO + ions through helium gas under the influence of an electrostatic field that is not necessarily weak. This interest leads us to solve a hierarchy of kinetic equations [5] by a threedimensional method of weighted residuals [19,20] in which the zero-order distribution function is the biMaxwellian distribution with a fraction, g, of the ions is characterized by a lower kinetic temperature, T~, and the remainder by a higher kinetic temperature, T 2:

k,M( v,J)

my2 ~

-

exp

2 "rrkT 1

j2 ] j2

2 kT 2

2 IkT 2

gm

+

2 kT I

(1 - g ) m

U2

2kT2

16)

and

g

2iT,

+ _ _1 - - g ] j 2 ,

17)

21kh

and where the 3-j symbols (:::), the normalized Laguerre (Sonine) polynomials ~(v+ ':/(W 2), and the spherical harmonics Yf(~) of the angles, ~, of v are the same as those used previously [25]. An important point about these basis functions is that they are not always real quantities, so that the expansion of the ion velocity distribution function in terms of them,

f[°l(v,j) =fBM(V,j)

Y" k,m.p,q, ~',t

2 IkT L

IIIU 2

W2=.__

(0) X f~..,.,,.(/.~., B( k , m ; p , q , s , t l v , j ) , ]

(18)

Here 1 is the moment of inertia of the ions, k is Boltzmann's constant, and m is the ions' mass. This method of weighted residuals converges rapidly when T L is approximately the temperature that characterizes the average energy of the ion-neutral interactions under the conditions of the experiment, and when the values of g and T2 are empirically adjusted to overcome the effects of partial ion runaway.

must provide for the possibility of imaginary or complex expansion coefficients, in order to end up calculating real quantities. Our previous manuscript [5] shows how a truncated set of the expansion coefficients f}{~.v.q..,., (and hence approximations to the transport coefficients and the ion distribution function) can be computed by matrix methods. Misprints, errors and additions in the previous work are described in the Appendix of this paper. The manuscript also shows how the matrix elements of the collision operator in

l -- g

- -

[

I11

~- -

i 3/2

~

+ 4wlkT2 ~ 2wkT2 ]

exp

(14)

12

L.A. Viehland et al. / Chemical Physics 211 (1996) 1 - 15

the kinetic equations can be computed from the transport cross-sections described above. We encountered many numerical difficulties when we asked our quadrature routines to evaluate the matrix elements only to an accuracy of 1%. Our reason for requesting this accuracy level was that we do not expect the cross-sections, and hence the integrands, to be more accurate than this. However, this apparently caused the integrations to stop 'too soon'; some unexplained structure in the integrated crosssections disappeared when we simply changed the requested accuracy to 0.1%. A further change was made in the numerical integrations, based on our experience with computing integrals that turned out to be quite small. In place of requiring all integrals to have a relative accuracy of 0.1%, we changed to calculating small cross-sections (those less than 1 × 10 -6 square bohr) using 256 quadrature points, whether or not the resulting value had converged.

6. Results Table 5 contains the reduced mobilities for NO + ions in helium gas at 300 K that we have calculated as a function of the ratio, E/N, of the electric field strength to the neutral gas number density below 20 Td (1 T d = 10 -2~ V m2). The calculations with g = 1.00 correspond to the use of a two-temperature

(only one ion temperature in addition to the gas temperature) approach [26,27] to the solution of the Boltzmann equation, except that here it is used for diatomic rather than atomic ions. Therefore, columns A1 and B1 should be the same, as should columns A2 and B2. They are, except for small disagreements that result from round-off and other numerical artifacts. Columns A I (or B l) and D1 in Table 5 agree within 0.1%, which exceeds the accuracy that we expect for the cross-sections used to compute these mobilities. Similar agreement is found between columns A2 (or B2) and D2. These values are therefore viewed as the 'correct' values obtained in the first and second approximations. However, the C mobilities are significantly different, both in first and second approximations. W h y ? The answer lies in the fact that the ion temperature T~ corresponding to the largest E/N value in Table 5 is 1600 K, corresponding to an energy of 0.0050 a.u. Therefore, the unusual behavior of the cross-sections for energies near 0.02 a.u., is probed by having a small fraction of the ions at 5 T~ but not when they are at only 1.5 T~. The C calculations place too much emphasis on energies above those relevant for mobilities below 20 Td, and hence the C mobilities are not further considered in this work. Fig. 3 shows a comparison of the calculated and measured mobilities. The agreement is very good, although the error estimates for the experimental

Table 5 Reduced mobilities, K o in c m 2 / V s, calculated in the present w o r k as a function o f the ratio, E / N in Td, of the electric field strength to the gas n u m b e r density. AI and A2 indicate the first and second a p p r o x i m a t i o n s calculated with g = 1.00 and T~ = 5T~, and BI and B 2 indicate those calculated with g - 1.00 and T 2 = 1.5Tp C I , C 2 , DI and D 2 are similar to AI, A2, BI and B 2 but with g - 0.99 E/N

AI

A2

BI

B2

0.30 2.93 4.30 5.48 6.60 7.72 8.85 10.02 11.26 12.56 13.96 15.46 17.09

22.457 22.424 22.386 22.353 22.308 22.269 22.2 l 6 22.164 22.092 22.014 21.911 21.793 21.650

22.474 22.447 22.415 22.392 22.355 22.328 22.201 22.251 22.968 22.153 22.092 22,036 21.953

22.457 22.423 22.386 22.352 22.308 22.268 22.215 22.163 22.091 22.013 21.910 21.791 21.648

22.474 22.446 22.415 22.391 22.354 22.327 22.200 22.250 22.969 22.152 22.090 22.030 21.947

CI

C2

22.371 22.294 22.224 22.145 22.073

22.392 22.358 22.365 22.385 22.421

21.905 21.803 21.694 21.561 21.411 21.237

22.589 22.259 23.506 22.358 22.585 22.152

DI

D2

22.300 22.259 22.204 22.150 22.077 21.997 21.893 21.773 21.628

22.347 22.320 22.192 22.242 23.025 22.144 22.083 22.023 21.933

L.A. Viehhmd et al. / Chemical Phy.vics 211 (1996) 1-15 v a l u e s are large since these data w e r e o b t a i n e d [7] i n c i d e n t a l to the m e a s u r e m e n t of i o n - m o l e c u l e reaction rate coefficients. Note that the f i r s t - a p p r o x i m a tion m o b i l i t i e s a p p e a r to be h e a d i n g t o w a r d v a l u e s at h i g h e r E / N that w o u l d lie b e l o w the e x p e r i m e n t a l v a l u e s a n d o u t s i d e their e r r o r bars, but that no similar t e n d e n c y is s h o w n by the s e c o n d - a p p r o x i m a t i o n m o b i l i t i e s . H o w e v e r , the d i f f e r e n c e b e t w e e n the first a n d s e c o n d a p p r o x i m a t i o n s b e c o m e s larger as E / N increases, i n d i c a t i n g that a b o v e 20 T d we w o u l d n e e d to c a l c u l a t e t h i r d - a p p r o x i m a t i o n m o b i l i t i e s in o r d e r to a c h i e v e v a l u e s c o n v e r g e d w i t h i n a b o u t 1%. S u c h c a l c u l a t i o n s are not p o s s i b l e with the c r o s s - s e c tions that we h a v e c o m p u t e d . T h e ' c o r r e c t ' , s e c o n d - a p p r o x i m a t i o n v a l u e s /'or the m o b i l i t y a n d o t h e r g a s e o u s ion t r a n s p o r t coefficients are g i v e n in T a b l e 6. T h e c o m p u t e r p r o g r a m a u t o m a t i c a l l y a d d e d the stars at the e n d o f s o m e of the lines, as a w a r n i n g a b o u t lack o f c o n v e r g e n c e . T h e v a l u e s at 11.26 a n d 18.86 Td a p p e a r p a r t i c u l a r l y u n t r u s t w o r t h y , a n d s h o u l d p r o b a b l y be d i s r e g a r d e d .

13

T h e m o b i l i t y is the last t r a n s p o r t c o e f f i c i e n t to be a f f e c t e d b y lack o f c o n v e r g e n c e , but e v e n it b e g i n s to f l u c t u a t e w i l d l y a b o v e 28 Td, w h i c h is w h y v a l u e s at h i g h e r E / N h a v e not b e e n reported. Note f r o m T a b l e 6 that the d i f f u s i o n c o e f f i c i e n t s and o t h e r t r a n s p o r t p r o p e r t i e s s h o u l d b e v i e w e d with s u s p i c i o n a b o v e 7 Td, particularly since in s o m e cases the a v e r a g e s o f s q u a r e d q u a n t i t i e s are n e g a t i v e . T r a n s p o r t p r o p e r t i e s i n v o l v i n g odd p o w e r s o f c o m p o n e n t s o f the a n g u l a r m o m e n t u m , like < J ) a n d ( J ~ ) , are identically equal to zero in o u r c a l c u l a tions, b e c a u s e o f the axial s y m m e t r y a b o u t the electric field direction. T h i s does not, h o w e v e r , rule out the p o s s i b i l i t y of rotational a l i g n m e n t o f the N O + ions as they drift t h r o u g h h e l i u m u n d e r the i n f l u e n c e o f an electric field, as is s h o w n b y the fact that "any J , M d e p e n d e n c e o n the f o r m o f the v e l o c i t y distribution is n e g l e c t e d ' in the s t e a d y - s t a t e m o d e l o f M e y e r et al. [28]. W e h a v e not a t t e m p t e d to c a l c u l a t e this a l i g n m e n t b e c a u s e , b a s e d on the e x p e r i m e n t a l results for N [ in He [29], o u r c a l c u l a t i o n s h a v e not con-

Table 6 Gaseous ion transport coefficients fk~rNO* ions in helium gas at 300 K, as functions of E/N in Td. K 0 is the reduced mobility, in cm2/V s. YD_ and ND, are the products of the gas number density and the ion diftiasion coefficients parallel and perpendicular to the electric field direction' in units of 1 0 t8 c m s.
E/N

Ko

ND_

ND,




<.1~)


0.30 2.93 4.30 5.48 6.60 7.72 8.85 10.02 I 1.26 12.56 13.96 15.46 17.09 18.86 20.79 22.91 25.24 27.81

22.474 22.446 22.415 22.391 22.354 22.327 22.200 22.250 22.969 22.152 22.090 22.030 21.947 21.249 21.452 21.168 21.034 20.866

15.598 15.971 16.392 16.878 17.402 17.999 19.365 19.308 28.327 20.689 21.350 22.085 21.467 14.690 19.247 13.714 60.541 14.473

15.596 15.761 15.956 16.196 16.479 16.831 17.899 17.788 14.252 19.299 20.415 22.054 23.411 17.574 24.421 28.348 20.856 37.328

0.018 0.176 0.259 0.330 0.397 0.463 0.528 0.599 0.695 0.748 0.829 0.915 1.008 1.077 1.198 1.303 1.426 1.559

0.083 0.116 0.155 0.199 0.251 0.312 0.384 0.465 0.578 0.676 0.809 0.966 1.147 1.280 1.564 1.811 2.315 2.564

0.083 0.084 0.085 0.087 0.088 0.090 0.()96 0.096 0.076 0.104 0. I 10 0. I 18 0.126 0.112 0.136 0.146 0.125 0.202

0.033 0.033 0.034 0.034 0.035 0.036 0.049 0.039 0.007 0.042 0.044 0.044 0.010 0.115 0.096 - 0.004 0.089 0.233

0.033 0.033 0.034 0.035 0.036 0.038 0.053 (/.043 0.016 0.052 (/.060 0.072 0.007 0.057 0.112 0. I 10 0.069 - (I.206

L.A. Viehland et al./Chemical Physics 211 (1996) 1 15

14

23i

have rather large uncertainties, we stopped at the second approximation of the kinetic theory. The calculated mobilities converged at E/N values up to 28 Td, while the other transport properties converged up to 8 Td. The limited range of convergence did not warrant calculation of rotational alignment effects or the full ion velocity distribution function, although it is certainly feasible to do this in future work. The good agreement shown in Fig. 3 between the calculated and measured mobilities below 20 Td indicates that the N O + - H e interaction potential calculated here is at least moderately accurate in the region probed by these data, i.e., for all polar angles but only for separations ranging from approximately 2.5 to 3.5 ,~.

22

Ko

o

21

Acknowledgements

q

i

10

15

20

25

E/N

Fig. 3. Reduced mobility, Ko in cm2/V s, as a function of the ratio, E/N in Td, of the electric field strength to the gas number density. The squares surrounded by error bars are the smoothed experimental values with the 7% accuracy estimated in Ref. [5]. The triangles are the present results in first approximation. The circles and small dots are the present results in second approximation using T2 equal to 5TI and 1.5 T~, respectively.

verged at values of E / N high enough for such alignment affects to be easily observed.

7. Discussion The present calculations are the first in which gaseous ion transport coefficients have been calculated for diatomic ions moving through atomic gases from an ab initio interaction potential that depends both upon the ion-atom separation and polar angle. The calculations are computationally intensive, particularly the classical-trajectory calculations of the transport cross-sections from the interaction potential, although less so than for the Li+-N2 or L i + - C O systems with their much deeper potential wells. For this reason, and because the experimental mobilities

The computational facilities used by one of us (ASD) are provided by SERC and by the University of Newcastle Research Committee. The work was partially supported by National Science Foundation Grant No. CHE-8814963.

Appendix A The following corrections and additions are needed in our previous work [5]. 1. The quantity (E'/E) q'/2 in Eq. (C.44) should be replaced by (E'r/Er) q'/i," 2. The quantity Y(q,4 ,k,m; j,]) in Eq. (C.44) should be replaced by Y(q,q',k,m;~f). 3. The power of e i in Eq. (C.39) should be t" + (q + q')/2, not l" + (q + q')/2. Note that when all three indices are zero, then the entire integral does not vanish at the ei = 0 endpoint. 4. The fifth index in the superscript list for Q in Eq. (C.39) should be 1' + 2B", not B" + 1'/2. 5. The 3-./" symbols in Eq. (C.30) add the constraint that l + L + E' must be even to the conditions listed in Eq. (C.33). 6. The equation referred to under Eq. (C.12) is Eq. (C.9), not Eq. (C.8). 7. The first quantity following the integral sign in Eq. (B.2) is hard to read; it should be Wf.

L.A. Viehhmd et al./Chemical Physics 211 (1996) 1 15

8. A more general version of Eq. (C.34) is that

X'(0,0lk,k)

= X'(0,01k,k)

[12]

F,

from which follows a more general version of Eq. (C.35):

[13] [14]

=

0

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