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Correct Expression of Material Derivative and Application to the Navier-Stokes

Equation

—– The solution existence condition of Navier-Stokes equation

Bo-Hua Sun1

1 School of Civil Engineering & Institute of Mechanics and Technology

Xi’an University of Architecture and Technology, Xi’an 710055, China http://imt.xauat.edu.cn

email: [email protected] (Dated: June 15, 2020)

The material derivative is important in continuum physics. This paper shows that the expression d

dt = ∂

∂t+ (v·∇), used in most literature and textbooks, is incorrect. This article presents correct expression of the material derivative, namely d(:)dt = ∂

∂t(:) +v·[∇(:)]. As an application, the form-solution of the Navier-Stokes equation is proposed. The form-form-solution reveals that the form-solution existence condition of the Navier-Stokes equation is that ”The Navier-Stokes equation has a solution if and only if the determinant of flow velocity gradient is not zero, namelydet(∇v)6= 0.”

Keywords: material derivative, velocity gradient, tensor calculus, tensor determinant, Navier-Stokes equa-tions, solution existence condition

In continuum physics, there are two ways of describ-ing continuous media or flows, the Lagrangian descrip-tion and the Eulerian descripdescrip-tion. In the Eulerian de-scription, the material derivative with respect to time must be defined. For mass density ρ(x, t), flow velocity v(x, t) = vkek, and stress tensor σ = σijei ⊗ej, the material derivatives are given by: dρdt = ∂ρ∂t +v1∂x∂ρ1 +

v2∂x∂ρ2 +v3∂x∂ρ3,,

dv

dt = ∂v

∂t +v1∂x∂v1 +v2∂x∂v2 +v3∂x∂v3, and

dt = ∂σ

∂t +v1 ∂σ

∂x1 +v2∂x∂σ2 +v3∂x∂σ3, respectively, where

t is time, x=xkek is position,ek is a base vector and

vk =∂x∂tk is the flow velocity.

In most popular textbooks, handbooks and encyclope-dia, such as Refs. 1–12, the above material derivatives are expressed as: dρdt = ∂ρ∂t+ (v·∇)ρ, dv

dt = ∂v

∂t+ (v·∇)v, and ddtσ = ∂∂tσ + (v·∇)v, where the gradient operator

∇=ek∂x

k.

To simplify the aforementioned equations further, a d-ifferential operator dtd =∂t∂ + (v·∇) is introduced. This operator is used by most fluid mechanics textbooks, in-cluding well-known graduate textbooks such as Landau & Lifshitz,[1, 2] Prandtl,[3, 4] Anderson,[5] Pope,[6] Cen-gel & Cimbala,[7], Kundu et al.[8], Woan [9], wikipedia [10, 11], Britannica [12] and even mathematical paper [13]. In the latest version of Landau & Lifshitz,[14] the material derivative of flow velocity is given in another form: dv

dt = ∂v

∂t + (v∇)v.

Besides the books mentioned above, there is a large amount of literature in fluid mechanics taking the same expressions as Refs. 1 and 14. This makes it difficult for readers to identify which expression for the materi-al derivative is correct, causing great confusion to both students and scholars.

Although some authors, such as Lighthill,[15] Batchelor,[16] Frisch,[17], Nhan & Nam [18], Xie,[19] and Zhao [20] have used the correct expression, it seems that most fluid mechanics textbooks and academic literature have adopted an incorrect expression for the material

derivative as in Ref. 1. Therefore, to revive the great influence of Landau in physics and fluid mechanics, we at-tempt to address this issue in this dedicated paper, where we revisit the material derivative to show why the oper-ators dtd = ∂t∂ + (v·∇) and expression ddtv = ∂∂tv+ (v∇)v are incorrect, and derive a correct expression by using standard tensor calculus [21–24].

In Landau & Lifshitz,[1] the material derivative is given as:

dx∂v ∂x +dy

∂v

∂y +dz ∂v

∂z = (dr·grad)v. (1)

Although Landau’s fluid mechanics is well known world-wide, the above expression is incorrect.

Proof: Since v ·grad = v ·∇ = (viei)· (∂jej) = vi,jei ·ej = vi,jδij = divv, and (v·grad)v = (v·∇)v= (vj,iei·ej)(vkek) =

δijvj,ivkek = vi,ivkek = (divv)v, where the divergence is divv = ∂v1

∂x1 +

∂v2

∂x2 +

∂v3

∂x3, so

(divv)v= (∂v1

∂x1 +

∂v2

∂x2 +

∂v3

∂x3)v. Thus:

(v·grad)v6=v1

∂v

∂x1 +v2

∂v

∂x2+v3

∂v

∂x3. (2)

In the latest version of Landau & Lifshitz,[14] for rea-sons which are unclear, the material derivative expression has been changed to ddtv = ∂∂tv+ (v∇)v; this is also incor-rect.

Proof: Sincev∇= (viei)(∂jej) =vi,jeiej,

(v∇)v = (vj,ieiej)(vkek) = (vj,ieiej)(vkek),

which indicates thatv∇is a 3rd-order tensor rather than a vector. Thus:

(v∇)v6=v1

∂v

∂x1+v2

∂v

∂x2 +v3

∂v

∂x3. (3)

(2)

To obtain the correct formulation of the material derivative, we perform some basic tensor calculus [21, 22]. The del operator is a vector differential operator, and de-fined by∇ =ei∂xi. An important note concerning the del operator ∇ is in order. Two types of gradients are used in continuum physics: left and right gradients. The left gradient is the usual gradient and the right gradient is the transpose of the forward gradient operator.

To see the difference between the left and right of gradients, consider a vector function A = Ai(x)ei. The left gradient of a vector A is ∇⊗A ≡ ej∂xj ⊗ (Aiei) = ∂A∂xjiej⊗ei=Ai,jej⊗ei, or written as∇A≡

ej∂xj(Aiei) = ∂A∂xjiejei = Ai,jejei. The right gradient of a vector A is A⊗∇ ≡ (Aiei)⊗ej∂xj = ∂A∂xjiei⊗

ej = Ai,jei ⊗ej, or written as A∇ ≡ (Aiei)ej∂xj = ∂Ai

∂xjeiej=Ai,jeiej, where Ai,j=

∂Ai

xj [21–24].

The gradient of a scalar function is a vector, the diver-gence of a vector-valued function is a scalar ∇·A, and the gradient of a vector-valued function is a second-order tensor ∇A. Although the del operator has some of the properties of a vector, it does not have them all, because it is an operator. For instance,∇·Ais a scalar (called the divergence ofA) whereasA·∇is a scalar differential operator, whereAis a vector. Thus the del operator∇

does not commute in this sense [21–24].

It worth to emphasise that the right gradient of a vec-tor A∇ is a more natural one, is often used in defining the deformation gradient tensor, displacement gradien-t gradien-tensor, and velocigradien-ty gradiengradien-t gradien-tensor. Igradien-t is clear gradien-thagradien-t A∇= (∇A)T.

With the above-mentioned understanding of tensor calculus, we material derivative expression for scalar, vec-tor and the 2nd order tensor as follows:

1. Mass densityρ=ρ(x, t) is a scalar-valued function of xand t and its differential is dρ= ∂ρ∂tdt+∂ρx· ∂x

∂tdt. For a scalar ∂ρx =ρ∇=∇ρ, sodρ= ∂ρ∂tdt+ (ρ∇)·vdt=

∂ρ

∂tdt+v·(∇ρ)dt, or, dividing both sides bydt,

dρ dt =

∂ρ

∂t + (ρ∇)·v= ∂ρ

∂t +v·(∇ρ). (4)

2. Flow velocityv=v(x, t) is a vector-valued function ofx andt and its differential isdv = ∂v

∂tdt+ ∂v

∂x·

∂x

∂tdt. For a vector ∂v

∂x = v ⊗∇ = v∇ = (∇v)

T. Strictly speaking, the right gradient of v should be written as v ⊗∇; here, in order to agree as far as possible with conventional presentation, we write v⊗∇ = v∇ and, similarly for the left gradient,∇⊗v =∇v. Hence (v∇)· v =v·(∇v) and dv = ∂∂tvdt+ (v∇)·vdt = ∂ρ∂tdt+v· (∇v)dt, or, dividing both sides bydt,

dv

dt = ∂v

∂t + (v∇)·v= ∂v

∂t +v·(∇v). (5)

3. The 2nd order stress tensorσ=σ(x, t) is a tensor-valued function of x and t and its differential is dσ =

∂σ

∂tdt+ ∂σ

∂x·

∂x

∂tdt. For an arbitrary tensor ∂σ

∂x =σ∇6=

(∇σ)T, hencedσ=∂∂tσdt+ (σ∇)·vdt, or dividing both sides bydtleads to dσ

dt = ∂σ

∂t+ (σ∇)·v. Since (σ∇)·v =

v·(∇σ),

dt = ∂σ

∂t +v·(∇σ). (6)

If an operator must be introduced for the material derivative, it should be in the following form:

d(:)

dt = ∂

∂t(:) +v·[∇(:)]. (7)

As an application, the Navier-Stokes equations of in-compressible flow can be expressed as follows:

∂v

∂t +v·(∇v) =−

1

ρ∇p+ν∇

2v, (8)

∇·v= 0. (9)

The Eq. 8 is momentums equation and Eq. 9 is mass conservation equation. In which, v(x, t) is flow velocity field,ρis constant mass density, p(x, t) is flow pressure,

ν is kinematical viscosity,tis time,x=xkek is position coordinates, ek is a base vector and v is flow velocity,

∇=ek∂x∂k is gradient operator, and∇

2=·. Applying the divergence operation to both sides of the momentum equation Eq.8 and use the mass conservation leads to a pressure equation:∇2·(p1) =ρ·(v·v) = −ρ{(∇v)2+ [∇(v∇)]·v}, where1=ekek is an identity tensor andv∇= (∇v)T.

The NavierõStokes existence and smoothness prob-lem is an open probprob-lem in mathematics [25], regardless of numerous abstract studies that have been done by math-ematicians. Now the question is that, is it possible to propose a simple criteria on the solution existence of the Navier-Stokes equation without complicated mathemat-ics.

In order to find some useful information from the Navier-Stokes equation, let’s have a look at the meaning ofv·(∇v) in Eq. 1. This term is called convective accel-eration that is caused by the flow velocity gradient. It is obvious that the convective accelerationv·(∇v) is the central point of the Navier-Stokes equations. Without the convective acceleration, the solution existence would not be a problem at all. The understanding on the con-vective term is quite important for the study on the so-lution existence should be focus onv·(∇v). Therefore, we attack the open problem from thev·(∇v).

Assuming the determinant of the velocity gradient is not zero, namely det∇v 6= 0, the form-solution of the Navier-Stokes momentum equation in Eq.(8) can be ex-pressed as follows

v=

ν∇2v1

ρ∇p− ∂v

∂t

·(∇v)−1, (10)

equivalently

v= (∇v)−T ·

ν∇2v1

ρ∇p− ∂v

∂t

(3)

equivalently

v =

∇·(ν∇v−p

ρ1)− ∂v

∂t

·(∇v)−1, (12)

equivalently

v = (∇v)−T·

∇·(ν∇v−p

ρ1)− ∂v

∂t

. (13)

The new formats of Naver-Stokes equations in Eqs. 10, 11, Eq.(12) and Eq.(13) have never been seen in litera-ture. They are formulated for the first time by Bo-Hua Sun [24]. Those form-solutions provide a rich information on the solution existence.

Therefore we have a conjecture as follows:

Conjecture 1 The 3D Navier-Stokes equation has a so-lution if and only if the determinant of flow velocity gra-dient is not zero, namely

det(∇v)6= 0.

Although we have successfully split the velocity field v from the convective term v·(∇v), the calculation of the inverse of the velocity gradient (∇v)−1 is still great challenge.

According to the Cayley-Hamilton theorem [22, 23, 26, 27], for the 2nd order tensor ∇v, the following polyno-mial holds:

(∇v)3−I1(∇v)2+I2∇v−I31=0, (14)

whereI1=tr(∇v) =∇·v, I2 = 12[(tr∇v)2−tr(∇v)2] andI3= det(∇v). Hence, for the case of det(∇v)6= 0, we have:

(∇v)−1= (∇v) 2I

1∇v+I21

det(∇v) . (15)

For incompressible flow, the divergence of velocity gra-dient is zero, namely, I1 = tr(∇v) = ∇·v = 0, thus

I2 = 12[(tr∇v)2−tr(∇v)2] = −12tr(∇v)2. Therefore, the inverse of the velocity gradient for incompressible flow takes a simpler form:

(∇v)−1= (∇v) 21

21tr(∇v) 2

det(∇v) . (16)

Therefore, the incompressible flow velocity field in Eq.(12) is then reduced to the following form:

v=

h

ν∇2v1 ρ∇p−

∂v

∂t

i

·[(∇v)21

21tr(∇v) 2]

det(∇v) ,

(17) where ∇v =vj,ieiej, (∇v)2 =∇v·∇v =vj,kvk,ieiej,

tr(∇v)2 = 1 : (v)2 = v

i,kvk,i and det(∇v) =

εijkv1,iv2,jv3,k, andεijk is permutation symbol. For steady flow, ∂∂tv =0, the Eq. 18 is reduced to

v=

h

ν∇2v1 ρ∇p

i

·[(∇v)21

21tr(∇v) 2]

det(∇v) , (18)

The great challenge to find solution of the Navier-Stokes equation are all from the existence of the velocity gradient∇v. The form solution in Eq.(18) reveals that the difficulty of finding a solution for N-S equations is because of existence of the nonlinear termv·(∇v), or in other words, due to the existence of the velocity field gradient ∇v. Accordingly, the solution of the Navier-Stokes equation will be blowup as det∇v tends to an infinitesimal, and has no solution when det∇v= 0.

The 2D N-S equations can be written as follows:

∂v1

∂t +v1 ∂v1

∂x1 +v2

∂v1 ∂x2 =ν(∂ 2v 1 ∂x2 1 +∂ 2v 1 ∂x2 2

)−1

ρ ∂p ∂x1 , (19) ∂v2

∂t +v1 ∂v2

∂x1 +v2

∂v2 ∂x2 =ν(∂ 2v 2 ∂x2 1 +∂ 2v 2 ∂x2 2

)−1

ρ ∂p ∂x1

.

(20)

wherevi,j= ∂x∂vij. The above equations can be expressed

in matrix format

∂ ∂t v1 v2 +

v1,1 v1,2

v2,1 v2,2

v1 v2 (21) =− 1 ρ ∂p ∂x1 1 ρ ∂p ∂x2 !

+ν∇2

v1

v2

, (22)

where the 2D Laplace operator∇2= ∂2 ∂x2

1

+∂2v2

∂x2 2

. The 2D velocity gradient is

∇v=

v1,1 v1,2

v2,1 v2,2

, (23)

its determinant is

det(∇v) =v1,1v2,2−v1,2v2,1, (24)

and the inverse of the 2D velocity gradient is thus

(∇v)−1= 1 det(∇v)

v2,2 −v1,2 −v2,1 v1,1

=

v2,2 −v1,2 −v2,1 v1,1

v1,1v2,2−v1,2v2,1

.

(25)

Therefore, from Eq. 21, the 2D flow velocity is given by

v1 v2 =

v2,2 −v1,2 −v2,1 v1,1

v1,1v2,2−v1,2v2,1

(ν∇2

∂t) v1 v2 −1 ρ

p,1

p,2

.

(26)

For the 2D steady flow, Eq.26 is reduced to

v1 v2 =

v2,2 −v1,2 −v2,1 v1,1

v1,1v2,2−v1,2v2,1

ν∇2

v1 v2 −1 ρ

p,1

p,2

.

(27)

(4)

Conjecture 2 The 2D Navier-Stokes equation has a so-lution if and only if the determinant of flow velocity gra-dient is not zero, namely det(∇v)6= 0, or equivalently

v1,1v2,2−v1,2v2,16= 0.

Concerning the geometrical and physical meaning of the conjectures, let’s try to give a basic interpretation. Assume thatd2X is small surface area of a moving fluid element with volumed3X, they become tod2xandd3x due to the velocity gradient det(∇v), respectively. Their relations are

d2x= det(∇v)(∇v)−T ·d2X, (28)

and the volume induced by the velocity gradient∇v is

d3x= det(∇v)d3X. (29)

From the relations in Eqs.28 and 29, both the surface aread2xand volumed3xinduced by the velocity gradient

∇v will shrink to a point as det(∇v)→0. If we image the finite surface area (d2x6=0) as a window that flow can go through, it means that, ifd2x=0, the window is closed and no flow can go through it.

Denoting the momentum flux density tensor in a vis-cous fluid Π = pI+ρv⊗v −µ∇v, and µ dynamical viscosity, according to Landau and Lifshitz [14], the lo-cal form of the equation of motion of the viscous fluid is

∂ρv

∂t +∇·Π=0, which can be rewritten in integral form

R∂ρv

∂t +∇·Π

d3X =0, and further simplified to

∂ ∂t

Z

ρvd3X+

I

Π·d2X =0, (30)

by Green’s formula.

Using Eqs.28 and 29, we can get an induced form of Eq.30 by the velocity gradient∇v as follows

∂ ∂t

Z ρvd3x det(∇v)+

I Π·(v)T ·d2x

det(∇v) =0. (31)

The Eq.31 will be invalid as det(∇v)→0. These might be viewed as another interpretation of the conjectures on solution existence.

In conclusion, the incorrect expression of material derivative operator dtd = ∂t∂ + (v·∇) is mainly because of the miscalculation ofv·∇; now we know that∇is a gra-dient operator rather than a vector, notingei·ej =δij, so that: (v·∇)v = [(eivi)·(ej∂j)]v = [vi,jei·ej]v = [vi,jδij]v=vi,iv= (∂v∂x11+

∂v2

∂x2 +

∂v3

∂x3)v, whilev·(∇v) =

v1∂x∂1+v2∂x∂2+v3∂x∂3, therefore (v·∇)v6=v·(∇v). The

correct material derivative operator should be defined as: d(:)

dt = ∂

∂t(:) +v·[∇(:)].

By taking into account of the importance of the con-vective termv·∇v, the conjectures on solution existence condition of Navier-Stokes equation have been proposed, which state that ”The Navier-Stokes equation has a solu-tion if and only if the determinant of flow velocity gradi-ent is not zero, namelydet(∇v)6= 0.” [24]. To be honest, this study on the solution existence is still in a very ba-sic stage. From future perspective, the mathematician-s mathematician-should be invited for comprehenmathematician-sive invemathematician-stigation and proof of the conjectures.

Availability of data: There are no data in this the-oretical article.

Conflict of interests: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper

Bo-Hua Sun: Conceptualization, Methodology, For-mulations, Formal analysis, Funding acquisition, Inves-tigation, Original draft preparation, Writing-Reviewing and Editing and all relevant works.

[1] L. D. Landau and E. M. Lifshitz,Fluid Mechanics (En-glish version) (1987).

[2] E. M. Lifshitz and L. P. Pitaevskii,Physical Kinetics (El-sevier (Singapore) Ltd, 2008)

[3] L. Prandtl,F¨uhrer durch die Str¨omungslehre, Herbert O-ertel (ed.) (Springer Vieweg, 2012).

[4] L. Prandtl,Prandtl’s essentials of fluid mechanics, Her-bert Oertel (ed.) (Springer-Verlag, 2004).

[5] J. D. Anderson,Computational Fluid Dynamics–The Ba-sics with Applications (The McGraw-Hill Companies, In-c., 1995).

[6] S. B. Pope, Turbulent Flows (Cambridge University Press, 2000).

[7] Y. A. Cengel and J. M. Cimbala,Fluid Mechanics: Fun-damentals and Applications (McGraw-Hill Education, Inc., 2020).

[8] P. K. Kundu, I. M. Cohen and D. R. Dowling, Fluid Mechanics (Elsevier, 2012).

[9] G. Woan,The Cambridge Handbook of Physics Formulas (Cambridge University Press, 2000)

[10] https://en.wikipedia.org/wiki/Gauge covariant derivative [11] https://en.wikipedia.org/wiki/Navier Stokes equations [12]

https://www.britannica.com/science/Navier-Stokes-equation

[13] T. Tao, Finite time blowup for an averaged three-dimensional Navier-Stokes equation, J. of the American Math. Society, 29, 3:601-674 (2016).

[14] L. D. Landau and E. M. Lifshitz,Fluid Mechanics (Rus-sian version) (2017).

[15] J. Lighthill, Waves in Fluids (Cambridge University Press, 1978)

(5)

(Cambridge University Press, 2007)

[17] U. Frisch, Turbulence (Cambridge University Press, 1995)

[18] P.T. Nhan and M.D. Nam,Understanding Viscoelastici-ty: An Introduction to Rheology (Springer-Verlag Berlin Heidelberg, 2013).

[19] X. C. Xie,Modern Tensor Analysis and Its Applications in Continuum Mechanics(Fudan University Press, 2014) [20] Y. P. Zhao,Lectures on Mechanics(Science Press, China,

2018)

[21] J.N. Reddy, An Introduction to Continuum Mechanics (Cambridge University Press NY, 2013).

[22] C. Truesdell,A First Course in Rational Continuum

Me-chanics (Academic Press, New York, 1977).

[23] Bo-Hua Sun, A new additive decomposition of velocity gradient, Physics of Fluids (Letter), 31, 061702 (2019). [24] B.H. Sun, Correct expression of material derivative in

continuum physics. Preprints 2020, 2020030030 (doi: 10.20944/preprints202003.0030.v3).

[25] C.L. Fefferman, Existence and smoothness of the Navier-Stokes equation, The millennium prize problems, Clay Math. Institute, pp. 57-67(2006).

[26] W.R. Hamilton, Lectures on Quaternions. Dublin(1853). [27] A. Cayley, A Memoir on the Theory of Matrices. Philos.

References

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