This paper was converted on www.awesomepapers.org from LaTeX by an anonymous user.
Want to know more? Visit the Converter page.

Use of the Basset coefficient in the calculation of the velocity of a spheroid slowing down in a viscous incompressible fluid after a sudden impulse

B. U. Felderhof ufelder@physik.rwth-aachen.de Institut für Theoretische Physik A
RWTH Aachen University
Templergraben 55
52056 Aachen
Germany
(July 30, 2025)
Abstract

The motion of a spheroid in a viscous incompressible fluid after a sudden small impulse in the direction of the symmetry axis is studied on the basis of the linearized Navier-Stokes equations. The time-dependence of the spheroid velocity follows by a Fourier transform from the frequency-dependence of the impedance involving friction coefficient, body mass, and added fluid mass. A term proportional to the square root of frequency in the asymptotic high frequency expansion of the impedance, with a Basset coefficient, describes the initial decay in time from the initial value determined by the effective mass. It is shown from numerical evidence based on the exact multipole expansion of the solution for the flow field in terms of spheroidal wavefunctions that the knowledge of the Basset coefficient is insufficient for a reliable estimate of the deviations from a simple two-pole approximation to the complete behavior in time. The two-pole approximation can be calculated from the effective mass and the steady state friction coefficient.

pacs:
47.10.A-, 47.15.G-, 47.63.mf, 83.10.Pp

I Introduction

The motion of a spheroid in a viscous incompressible fluid, after a sudden small impulse directed along the symmetry axis, may in principle be calculated from the linearized Navier-Stokes equations for fluid velocity and pressure, in combination with a boundary condition for the flow velocity at the surface of the spheroid. In the following we assume that the no-slip boundary condition holds. For a small body the no-slip condition must be relaxed and replaced by a partial slip boundary condition 1 .

The added mass tensor, which together with the body mass determines the initial velocity after the impulse, has long been known from the general expressions for an ellipsoid 2 . Similarly, the steady state friction tensor, which determines the steady state velocity for a constant force, is also known for the general ellipsoid 2 . The complete time-dependence of the velocity after a sudden impulse follows in principle by Fourier transform from the frequency-dependence of the friction tensor, but this is not known for a general ellipsoid. For axial motion of a spheroid the frequency-dependent friction coefficient can be found in principle from a set of coupled equations for the multipole moments of the force density induced on the spheroid, as shown first by Lai and Mockros 3 . It was shown by Lawrence and Weinbaum 4 , that the equations can be solved efficiently by truncation and matrix inversion.

At low frequency the friction coefficient for axial motion is linear in the square root of frequency, with a coefficient which can be found from the friction coefficient at zero frequency 5 ,6 . As a consequence of this relation the velocity relaxation function shows a t3/2t^{-3/2} long-time tail, independent of shape, size, and mass density of the spheroid. The transient effects on the short and intermediate time scale are less well known.

For the case of a sphere, Stokes 7 derived a simple explicit formula for the frequency-dependent friction coefficient. The impedance of a sphere is quadratic in the square root of frequency. The term linear in the square root is relevant both at low and at high frequency. The corresponding motion of a sphere has been studied by Boussinesq 8 . For a spheroid, the asymptotic behavior of the impedance at high frequency is given by a term linear in frequency, with coefficient given by the sum of spheroid mass and added fluid mass, and a term proportional to the square root of frequency, with a Basset coefficient. Lawrence and Weinbaum 4 calculated the latter from an expression derived by Landau and Lifshitz 9 and Batchelor 10 for a body of arbitrary shape. The Basset coefficient differs from the coefficient of the term linear in the square root of frequency at low frequency. In previous work we have calculated the Basset coefficient for a general ellipsoid for the three principal directions 11 .

The steady state friction coefficient and the effective mass are sufficient for the construction of a simple, approximate expression for the complex admittance, showing two poles in the complex plane of the square root of frequency. On the basis of their numerical work Lawrence and Weinbaum suggested a three-pole expression for the complex admittance corresponding to the axial motion of a spheroid, involving the steady-state friction coefficient, the effective mass, and the Basset coefficient 4 . It has been suggested that the approximate expression provides an adequate approximation to the actual admittance 12 ,13 . In the following we examine this idea by comparison with a calculation of the admittance on the basis of the method of Padé approximants 14 . Our conclusion is that the simple two-pole expression is quite useful, and that the small deviations from the two-pole approximation are not well described by the Lawrence-Weinbaum expression.

II Admittance

We consider a prolate or oblate spheroid of mass mpm_{p} immersed in a viscous incompressible fluid of shear viscosity η\eta, mass density ρ\rho. The fluid is assumed to fill the whole outer space, and a no-slip boundary condition holds at the surface of the spheroid. The spheroid and the fluid are at rest for t<0t<0. We choose a cylindrical frame of coordinates (r,φ,z)(r,\varphi,z) such that the center of the spheroid at rest is at the origin, and the zz axis is the axis of symmetry. Furthermore rr is the radial distance from the axis, and φ\varphi is the azimuthal angle. We follow the convention of Happel amd Brenner 15 , and denote the longest semi-axis by aa and the shortest by bb in both the prolate and the oblate case. At time t=0t=0 a sudden impulse 𝑺=S𝒆z\mbox{\boldmath$S$}=S\mbox{\boldmath$e$}_{z} in the direction of the symmetry axis is imparted to the spheroid, corresponding to the applied force

𝑭(t)=S𝒆zδ(t).\mbox{\boldmath$F$}(t)=S\mbox{\boldmath$e$}_{z}\delta(t). (1)

The impulse is assumed to be sufficiently small that the resulting flow velocity 𝒗(𝒓,t)\mbox{\boldmath$v$}(\mbox{\boldmath$r$},t) and pressure p(𝒓,t)p(\mbox{\boldmath$r$},t) can be assumed to satisfy the linearized Navier-Stokes equations

ρ𝒗t=η2𝒗p,𝒗=0.\rho\frac{\partial\mbox{\boldmath$v$}}{\partial t}=\eta\nabla^{2}\mbox{\boldmath$v$}-\nabla p,\qquad\nabla\cdot\mbox{\boldmath$v$}=0. (2)

The flow velocity 𝒗v tends to zero at infinity, and the pressure pp tends to a constant pstp_{st}. We are interested in the corresponding velocity 𝑼(t)=U(t)𝒆z\mbox{\boldmath$U$}(t)=U(t)\mbox{\boldmath$e$}_{z} of the spheroid.

The equation of motion for the spheroid reads

mpdUdt=K(t)+F(t),m_{p}\frac{dU}{dt}=K(t)+F(t), (3)

where K(t)K(t) is the hydrodynamic force exerted by the fluid, which may be calculated from the fluid stress tensor. In Fourier transform the equation becomes

iωmpUω=Kω+Fω.-i\omega m_{p}U_{\omega}=K_{\omega}+F_{\omega}. (4)

Since KωK_{\omega} is linear in UωU_{\omega} this may be resolved to the form

Uω=𝒴(ω)Fω,U_{\omega}=\mathcal{Y}(\omega)F_{\omega}, (5)

with admittance 𝒴(ω)\mathcal{Y}(\omega). The latter may be cast in the form

𝒴(ω)=[iω(mp+ma)+ζ(ω)]1.\mathcal{Y}(\omega)=\big{[}-i\omega(m_{p}+m_{a})+\zeta(\omega)\big{]}^{-1}. (6)

Here mam_{a} is the added mass, which follows from the high-frequency behavior. The friction coefficient ζ(ω)\zeta(\omega) is at most linear in ω\sqrt{\omega} at high frequency. The impedance is the inverse of the admittance.

The added mass mam_{a} follows from the theory of potential flow, and is well known 2 . The friction coefficient at zero frequency follows from the solution of the steady state Stokes equations. It takes the form

ζ(0)=6πηR,\zeta(0)=6\pi\eta R, (7)

where RR has the dimension length. Its explicit expression is also well known 2 .

For a sphere of radius aa the friction coefficient takes the simple form 7

ζ(ω)=6πηa(1+αa),\zeta(\omega)=6\pi\eta a(1+\alpha a), (8)

where α=iωρ/η,Reα>0\alpha=\sqrt{-i\omega\rho/\eta},\;\mathrm{Re}\;\alpha>0. Similarly, for a spheroid the friction coefficient can be expanded in powers of α\alpha as

ζ(ω)=ζ(0)+ζ(1)α+ζ(2)α2+O(α3).\zeta(\omega)=\zeta^{(0)}+\zeta^{(1)}\alpha+\zeta^{(2)}\alpha^{2}+O(\alpha^{3}). (9)

The term linear in α\alpha can be expressed in terms of the coefficient at zero frequency ζ(0)=ζ(0)\zeta(0)=\zeta^{(0)} as

ζ(1)=16πηζ(0)2.\zeta^{(1)}=\frac{1}{6\pi\eta}\zeta(0)^{2}. (10)

A similar theorem in tensor form holds for a body of arbitrary shape 5 ,6 .

The first term in the asymptotic expansion of ζ(ω)\zeta(\omega) in powers of α1\alpha^{-1} is linear in α\alpha,

ζ(ω)=6πηαa2B+O(1),asα,\zeta(\omega)=6\pi\eta\alpha a^{2}B+O(1),\qquad\mathrm{as}\;\alpha\rightarrow\infty, (11)

where BB is the dimensionless Basset coefficient 16 ,4 . For a sphere B=1B=1 from Eq. (8). The explicit expression for an ellipsoid can be evaluated from the theory of potential flow 2 by use of an argument due to Landau and Lifshitz 9 and to Batchelor 10 . The expression for an oblate spheroid was derived by Lawrence and Weinbaum 4 . It agrees with the one derived for a general ellipsoid 11 . The corresponding expression for a prolate spheroid has also been derived 11 ,12 .

It is convenient to write the admittance in the form

𝒴(ω)=[iωmp+𝒴0(ω)1]1,𝒴0(ω)=[iωma+ζ(ω)]1,\mathcal{Y}(\omega)=\big{[}-i\omega m_{p}+\mathcal{Y}_{0}(\omega)^{-1}\big{]}^{-1},\qquad\mathcal{Y}_{0}(\omega)=\big{[}-i\omega m_{a}+\zeta(\omega)\big{]}^{-1}, (12)

where 𝒴0(ω)\mathcal{Y}_{0}(\omega) is related to the Fourier transform of the hydrodynamic force by

Uω=𝒴0(ω)Kω.U_{\omega}=-\mathcal{Y}_{0}(\omega)K_{\omega}. (13)

It clearly is independent of the mass mpm_{p}.

We define the viscous relaxation time τv=a2ρ/η\tau_{v}=a^{2}\rho/\eta, and the corresponding complex variable λ=iωτv=αa\lambda=\sqrt{-i\omega\tau_{v}}=\alpha a. The function 𝒴0(ω)\mathcal{Y}_{0}(\omega) may be cast in the form 11

𝒴0(ω)=16πη1R+(R2/a)λ+M0λ2+aλ2ψ(λ),\mathcal{Y}_{0}(\omega)=\frac{1}{6\pi\eta}\frac{1}{R+(R^{2}/a)\lambda+M_{0}\lambda^{2}+a\lambda^{2}\psi(\lambda)}, (14)

where M0=ma/(6πa2ρ)M_{0}=m_{a}/(6\pi a^{2}\rho), and the function ψ(λ)\psi(\lambda) tends to zero at large λ\lambda. For a sphere R=a,M0=a/9R=a,\;M_{0}=a/9, and ψ(λ)=0\psi(\lambda)=0. In that case the expression for 𝒴0(ω)\mathcal{Y}_{0}(\omega) has just two poles in the complex λ\lambda plane.

More generally, the function ψ(λ)\psi(\lambda) may be written as a continued fraction

ψ(λ)=A01+A1λ1+A2λ.\psi(\lambda)=\frac{A_{0}}{1+\frac{A_{1}\lambda}{1+A_{2}\lambda...}}. (15)

A Padé approximant to the exact function is obtained by breaking off at some level. A three-pole approximation to the admittance is found by putting

ψ3(λ)=A01+A1λ\psi_{3}(\lambda)=\frac{A_{0}}{1+A_{1}\lambda} (16)

with suitably chosen coefficients A0,A1A_{0},\;A_{1}. In order to agree with the high-frequency behavior given by Eq. (11) we must have

A0A1=BR2a2\frac{A_{0}}{A_{1}}=B-\frac{R^{2}}{a^{2}} (17)

in the three-pole approximation. Lawrence and Weinbaum 4 have suggested on the basis of their explicit calculations for a spheroid that a good approximation to the admittance 𝒴0(ω)\mathcal{Y}_{0}(\omega) is found by use of Eq. (16) with A1=1A_{1}=1 and the coefficient A0A_{0} calculated from the Basset coefficient BB by use of Eq. (17). In the following we examine this suggestion for a test case, for both an oblate and a prolate spheroid.

III Hydrodynamic force

The calculation will be based on the solution of the linearized Navier-Stokes equations Eq. (2) after a Fourier transform in time. By axial symmetry the flow velocity and the pressure can be derived from a scalar Stokes stream function. The partial differential equation for the stream function separates in spheroidal coordinates, and the solution can be expressed as an infinite sum of products of radial and angular spheroidal wavefunctions 4 . In the calculation we have used spheroidal wavefunctions as programmed in Mathematica 6.

It has been shown by Lawrence and Weinbaum 16 that the hydrodynamic force KωK_{\omega} can be evaluated from the behavior of the stream function at large distance from the origin, i.e. from the value of the lowest order multipole moment. The exact set of coupled multipole equations has been derived by Lai and Mockros 3 . It was shown by Lawrence and Weinbaum 4 that the infinite set of linear coupled multipole equations can be solved approximately by truncation and matrix inversion.

It is convenient to define the dimensionless reduced hydrodynamic force G(ω)G(\omega) by

G(ω)=Kω/K0,G(0)=1.G(\omega)=K_{\omega}/K_{0},\qquad G(0)=1. (18)

It follows from Eq. (13) that

G(ω)=6πηR𝒴0(ω).G(\omega)=6\pi\eta R\mathcal{Y}_{0}(\omega). (19)

We denote the corresponding expression obtained by putting ψ(λ)=0\psi(\lambda)=0 in Eq. (14) as

G2p0(ω)=RR+(R2/a)λ+M0λ2.G_{2p0}(\omega)=\frac{R}{R+(R^{2}/a)\lambda+M_{0}\lambda^{2}}. (20)

This is a two-pole approximation to the actual function. We call this a two-pole approximation, since the function has two poles in the complex ω\sqrt{\omega} plane. The deviation from the exact function is characterized by the function ψ(λ)\psi(\lambda) in Eq. (14).

We have used the exact multipole equations to calculate the function ψ(λ)\psi(\lambda) at a chosen set of positive values λj\lambda_{j} corresponding to values on the positive imaginary axis of the complex frequency plane. As test cases we have chosen a prolate and an oblate spheroid with aspect ratio b/a=0.5b/a=0.5. It follows from Table 4-26.1 in Happel and Brenner 15 that the corresponding value of the steady-state friction coefficient is ζ(0)=0.9053×6πηa\zeta(0)=0.9053\times 6\pi\eta a in the oblate case, and ζ(0)=1.2039×6πηb\zeta(0)=1.2039\times 6\pi\eta b in the prolate case. For values of the aspect ratio b/ab/a closer to unity the correction ψ(λ)\psi(\lambda) is very small, and hardly worth calculating. For values of the aspect ratio much less than unity a large number of multipoles must be included to achieve convergence, and the numerical calculation becomes more demanding.

In Table I we list the values ψj=ψ(λj)\psi_{j}=\psi(\lambda_{j}) at the chosen values λ1=0.2,λ2=0.4,λ3=0.7,λ4=1,λ5=1.5,λ6=2\lambda_{1}=0.2,\;\lambda_{2}=0.4,\;\lambda_{3}=0.7,\;\lambda_{4}=1,\;\lambda_{5}=1.5,\;\lambda_{6}=2, and compare with the corresponding values of the function

ψLW(λ)=BR2/a21+λ,\psi_{LW}(\lambda)=\frac{B-R^{2}/a^{2}}{1+\lambda}, (21)

corresponding to the approximation of Lawrence and Weinbaum 4 . For the oblate spheroid there is fair agreement, but for the prolate spheroid the LW-approximation yields values with the wrong sign. The numerator in Eq. (21) is negative for the prolate spheroid. It is positive for an oblate spheroid.

IV Velocity relaxation function

In this section we derive approximate expressions for the velocity relaxation function based on the results derived above, and show numerical results for a prolate and an oblate spheroid of aspect ratio b/a=0.5b/a=0.5. By inversion of the Fourier transform in Eq. (5) we find

U(t)=Ψ(t)S,t>0.U(t)=\Psi(t)S,\qquad t>0. (22)

The initial value of the velocity relaxation function Ψ(t)\Psi(t) is

Ψ(0+)=1m,m=mp+ma,\Psi(0+)=\frac{1}{m^{*}},\qquad m^{*}=m_{p}+m_{a}, (23)

with effective mass mm^{*}. The initial value is less than 1/mp1/m_{p} due to loss of momentum to infinity via longitudinal sound waves 17 . The low frequency behavior of the friction tensor, given by Eq. (9), corresponds to the long-time behavior 18

Ψ(t)ρ12(πηt)3/2,ast,\Psi(t)\approx\frac{\sqrt{\rho}}{12(\pi\eta t)^{3/2}},\qquad\mathrm{as}\;t\rightarrow\infty, (24)

independent of the shape and size of the spheroid and its mass density ρp\rho_{p}.

We write the relaxation function in the form

Ψ(t)=1mγ(t),\Psi(t)=\frac{1}{m^{*}}\gamma(t), (25)

with dimensionless function γ(t)\gamma(t) with initial value γ(0)=1\gamma(0)=1. The function has the one-sided Fourier transform

Γ(ω)=0eiωtγ(t)𝑑t=m𝒴(ω).\Gamma(\omega)=\int^{\infty}_{0}e^{i\omega t}\gamma(t)\;dt=m^{*}\;\mathcal{Y}(\omega). (26)

The simplest estimate of the function γ(t)\gamma(t) is the exponential exp(t/τM)\exp(-t/\tau_{M}), with mean relaxation time τM=m/(6πηR)\tau_{M}=m^{*}/(6\pi\eta R), but this violates the long-time behavior given by Eq. (24).

An approximate relaxation function which accounts for the initial value, the mean relaxation time τM\tau_{M}, and the long-time behavior (24), is given by the approximate two-pole expression

Γ2p(ω)=a2ρηMR+(R2/a)λ+Mλ2,\Gamma_{2p}(\omega)=\frac{a^{2}\rho}{\eta}\;\frac{M}{R+(R^{2}/a)\lambda+M\lambda^{2}}, (27)

where M=m/(6πa2ρ)M=m^{*}/(6\pi a^{2}\rho) has the dimension length. In the two-pole approximation the function γ(t)\gamma(t) takes the approximate form 18

γ2p(t)=1σ24[v+w(iv+t/τM)vw(ivt/τM)],\gamma_{2p}(t)=\frac{1}{\sqrt{\sigma^{2}-4}}\;\big{[}v_{+}w(-iv_{+}\sqrt{t/\tau_{M}})-v_{-}w(-iv_{-}\sqrt{t/\tau_{M}})\big{]}, (28)

where

σ=6πρR3m,v±=12σ±12σ24,\sigma=\sqrt{\frac{6\pi\rho R^{3}}{m^{*}}},\qquad v_{\pm}=-\frac{1}{2}\sigma\pm\frac{1}{2}\sqrt{\sigma^{2}-4}, (29)

and w(z)=exp(z2)erfc(iz)w(z)=\exp(-z^{2})\mathrm{erfc}(-iz).

The two-pole approximation is determined by the effective mass and the friction coefficient at zero frequency. In order to find the actual behavior of the velocity relaxation function, we must take account of the function ψ(λ)\psi(\lambda), defined in Eq. (14). The approximation of Lawrence and Weinbaum, corresponding to Eq. (21), leads to a three-pole approximation to the velocity relaxation function, which we denote as γLW(t)\gamma_{LW}(t). More generally, the time-dependence of the reduced velocity relaxation function in an NN-pole approximation is given by 14

γN(t)=k=1NRkvkw(ivkt/τv),\gamma_{N}(t)=\sum^{N}_{k=1}R_{k}v_{k}w(-iv_{k}\sqrt{t/\tau_{v}}), (30)

where {vk}\{v_{k}\} are the NN poles of the one-sided Fourier transform ΓN(ω)\Gamma_{N}(\omega) in the complex λ\lambda plane, and {Rk}\{R_{k}\} are the residues.

The function ΓN(ω)\Gamma_{N}(\omega) is found numerically from a Padé approximant to the function ψ(λ)\psi(\lambda) determined by the values of the reduced hydrodynamic force G(ω)G(\omega) at selected positive values {λj}\{\lambda_{j}\}. For example, the six values listed in Table I are sufficient to determine a 5-pole approximation γ5(t)\gamma_{5}(t). In this case the Padé approximant to the function ψ(λ)\psi(\lambda) is the ratio of a cubic and a quintic polynomial in λ\lambda.

We find numerically that for aspect ratio b/a=0.5b/a=0.5 it suffices to include multipoles of order n=17n=17, in the notation of Lawrence and Weinbaum 4 . This corresponds to a set of nine coupled multipole equations, since only odd multipoles occur. We have calculated the values of ψ(λ)\psi(\lambda) at eight positive values {λj}\{\lambda_{j}\}, corresponding to a six-pole approximation γ6(t)\gamma_{6}(t). It turns out that in fact two of the residues are negligibly small, so that γ(t)\gamma(t) is represented accurately by four pole contributions. The larger number of values {λj}\{\lambda_{j}\} allow a more accurate determination of the relevant residues and poles. The difference between the approximations γ5(t)\gamma_{5}(t) and γ6(t)\gamma_{6}(t) cannot be seen graphically.

In Fig. 1 we plot the ratio γ6(t)/γ2p(t)\gamma_{6}(t)/\gamma_{2p}(t) as a function of log10(t/τv)\log_{10}(t/\tau_{v}) for an oblate spheroid with aspect ratio b/a=0.5b/a=0.5 and vanishing mass density ρp=0\rho_{p}=0, and compare with the approximation of Lawrence and Weinbaum calculated from Eq. (21). In Fig. 2 we present the corresponding plots for a neutrally buoyant spheroid with ρp=ρ\rho_{p}=\rho. In Figs. 3 and 4 we present similar plots for a prolate spheroid with aspect ratio b/a=0.5b/a=0.5 and mass densities ρp=0\rho_{p}=0 and ρp=ρ\rho_{p}=\rho, respectively. It turns out that for the oblate spheroid the Lawrence-Weinbaum approximation agrees qualitatively, but that for the prolate spheroid it is qualitatively wrong. In both cases the deviation from the two-pole approximation γ2p(t)\gamma_{2p}(t) is less than one percent.

V Discussion

The frequency-dependent admittance of a prolate or oblate spheroid can be analyzed efficiently by the method of Padé approximants applied to the approximate solution of the exact set of coupled equations for the multipole moments of the hydrodynamic force density. The method leads to an approximate representation of the admittance as a ratio of two polynomials in the square root of frequency. Hence one can evaluate the time-dependent velocity relaxation function as a sum of ww functions.

We have applied the method to a prolate or oblate spheroid of aspect ratio b/a=0.5b/a=0.5 for two values of the spheroid mass density, and have compared the numerical results with those calculated from the approximation proposed by Lawrence and Weinbaum 4 . The comparison is shown in Figs. 1-4. The figures show that for the cases considered the deviation from the two-pole approximation is quite small, and not well described by the approximation of Lawrence and Weinbaum 4 , based on just the Basset coefficient.

The elaborate calculation in terms of spheroidal wavefunctions leads to only a small deviation from the result which may be calculated from the steady state friction coefficient and the effective mass, as given by the classical expressions for a general ellipsoid 2 ,11 . Presumably an exact calculation for an ellipsoid would lead to the same conclusion in that case. For many practical purposes 19 the two-pole approximation to the admittance, as determined from steady state friction coefficient and effective mass, will be sufficient. The use of only the Basset coefficient for a calculation of the deviations from the two-pole approximation on the intermediate timescale is questionable.

References

  • (1) C. M. Hu and R. Zwanzig, ”Rotational friction coefficients for spheroids with the slipping boundary condition,” J. Chem. Phys. 60, 4354 (1974).
  • (2) H. Lamb, Hydrodynamics (Dover, New York, 1945).
  • (3) R. Y. S. Lai and L. F. Mockros, ”The Stokes-flow drag on prolate and oblate spheroids during axial translatory accelerations,” J. Fluid Mech. 52, 1 (1972).
  • (4) C. J. Lawrence and S. Weinbaum, ”The unsteady force on a body at low Reynolds number; the axisymmetric motion of a spheroid,” J. Fluid Mech. 189, 463 (1988).
  • (5) W. E. Williams, ”A note on slow vibrations in a viscous fluid,” J. Fluid Mech. 25, 589 (1966).
  • (6) B. Cichocki and B. U. Felderhof, ”Long-time collective motion of rigid bodies immersed in a viscous fluid,” Physica A 211, 25 (1994).
  • (7) G. G. Stokes, ”On the effect of internal friction of fluids on the motion of pendulum,” Trans. Cambridge Phil. Soc. 9, 8 (1851).
  • (8) J. Boussinesq, ”Sur la résistance qu’oppose un liquide indéfini en repos,” Comptes Rendus Acad. Sci. 100, 935 (1885).
  • (9) L. D. Landau and E. M. Lifshitz, Fluid Mechanics (Pergamon Press, New York, 1959), Eq. (24.14).
  • (10) G. K. Batchelor, An Introduction to Fluid Dynamics (Cambridge University Press, Cambridge, 1967).
  • (11) B. U. Felderhof, ”Velocity relaxation of an ellipsoid immersed in a viscous incompressible fluid,” Phys. Fluids 25, 013101 (2013).
  • (12) M. Loewenberg, ”Stokes resistance, added mass, and Basset force for arbitrarily oriented, finite-length cylinders,” Phys. Fluids A 5, 765 (1993).
  • (13) W. Zhang and H. A. Stone, ”Oscillatory motions of spherical disks and nearly spherical particles in viscous flows,” J. Fluid Mech. 367, 329 (1998).
  • (14) B. Cichocki and B. U. Felderhof, ”Slow dynamics of linear relaxation systems,” Physica A 211, 165 (1994).
  • (15) J. Happel and H. Brenner, Low Reynolds number hydrodynamics (Noordhoff, Leyden, 1973).
  • (16) C. J. Lawrence and S. Weinbaum, ”The force on an axisymmetric body in linearized, time-dependent motion,” J. Fluid Mech. 171, 209 (1986).
  • (17) R. Zwanzig and M. Bixon, ”Compressibility effects in the hydrodynamic theory of Brownian motion,” J. Fluid Mech. 69, 21 (1975).
  • (18) B. Cichocki and B. U. Felderhof, ”Velocity autocorrelation function of interacting Brownian particles,” Phys. Rev. E 51, 5549 (1995).
  • (19) T. Franosch, M. Grimm, M. Belushkin, F. M. Mor, G. Foffi, L. Forró, and S. Jeney, ”Resonances arising from hydrodynamic memory in Brownian motion,” Nature 478, 85 (2011).
Table 1:
λ\lambda 0.20.2 0.40.4 0.70.7 11 1.51.5 22
oblate\mathrm{oblate} 105ψ10^{5}\psi 521521 473473 409409 358358 294294 247247 ​​​
105ψLW10^{5}\psi_{LW} 511511 438438 361361 307307 245245 204204 ​​​
prolate\mathrm{prolate} 105ψ10^{5}\psi 5858 4545 2727 1515 11 8-8 ​​​
105ψLW10^{5}\psi_{LW} 248-248 212-212 175-175 149-149 119-119 99-99 ​​​

Table caption

Table of values of the function ψ(λ)\psi(\lambda) at selected values of λ\lambda for an oblate and a prolate spheroid of aspect ratio b/a=0.5b/a=0.5, as calculated from the set of coupled multipole equations, compared with the Lawrence-Weinbaum approximation given by Eq. (21).

Fig. 1

Plot of the ratio γ6(t)/γ2p(t)\gamma_{6}(t)/\gamma_{2p}(t) as a function of log10(t/τv)\log_{10}(t/\tau_{v}) for an oblate spheroid with aspect ratio b/a=0.5b/a=0.5 and mass density ρp=0\rho_{p}=0 (solid curve), compared with the corresponding ratio γLW(t)/γ2p(t)\gamma_{LW}(t)/\gamma_{2p}(t), as given by the Lawrence-Weinbaum approximation Eq. (21) (dashed curve).

Fig. 2

Plot of the ratio γ6(t)/γ2p(t)\gamma_{6}(t)/\gamma_{2p}(t) as a function of log10(t/τv)\log_{10}(t/\tau_{v}) for an oblate spheroid with aspect ratio b/a=0.5b/a=0.5 and mass density ρp=ρ\rho_{p}=\rho (solid curve), compared with the corresponding ratio γLW(t)/γ2p(t)\gamma_{LW}(t)/\gamma_{2p}(t), as given by the Lawrence-Weinbaum approximation Eq. (21) (dashed curve).

Fig. 3

Plot of the ratio γ6(t)/γ2p(t)\gamma_{6}(t)/\gamma_{2p}(t) as a function of log10(t/τv)\log_{10}(t/\tau_{v}) for a prolate spheroid with aspect ratio b/a=0.5b/a=0.5 and mass density ρp=0\rho_{p}=0 (solid curve), compared with the corresponding ratio γLW(t)/γ2p(t)\gamma_{LW}(t)/\gamma_{2p}(t), as given by the Lawrence-Weinbaum approximation Eq. (21) (dashed curve).

Fig. 4

Plot of the ratio γ6(t)/γ2p(t)\gamma_{6}(t)/\gamma_{2p}(t) as a function of log10(t/τv)\log_{10}(t/\tau_{v}) for a prolate spheroid with aspect ratio b/a=0.5b/a=0.5 and mass density ρp=ρ\rho_{p}=\rho (solid curve), compared with the corresponding ratio γLW(t)/γ2p(t)\gamma_{LW}(t)/\gamma_{2p}(t), as given by the Lawrence-Weinbaum approximation Eq. (21) (dashed curve).

Refer to caption
Figure 1:
Refer to caption
Figure 2:
Refer to caption
Figure 3:
Refer to caption
Figure 4: