1 Introduction

Let Ω R 3 be a bounded domain with smooth boundary Ω, and let ν be the unit outward normal vector on Ω. We consider the regularity criterion to the density-dependent incompressible nematic liquid crystal model as follows [14]:

divu=0,
(1.1)
t ρ+div(ρu)=0,
(1.2)
t (ρu)+div(ρuu)+πΔu=(dd),
(1.3)
t d+ud+ ( | d | 2 1 ) dΔd=0,
(1.4)

in (0,)×Ω with initial and boundary conditions

(ρ,u,d)(,0)=( ρ 0 , u 0 , d 0 )in Ω,
(1.5)
u=0, ν d=0on Ω,
(1.6)

where ρ denotes the density, u the velocity, π the pressure, and d represents the macroscopic molecular orientations, respectively. The symbol dd denotes a matrix whose (i,j)th entry is i d j d, and it is easy to find that dd= d T d.

When d is a given constant vector, then (1.1)-(1.3) represent the well-known density-dependent Navier-Stokes system, which has received many studies; see [57] and references therein.

When ρ=1, Guillén-González et al. [8] proved the blow-up criterion

0 T ( u ( t ) L q 2 q q 3 + d ( t ) L q 2 q q 3 ) dt<with 3<q
(1.7)

and 0<T<.

It is easy to prove that the problem (1.1)-(1.6) has a unique local-in-time strong solution [6, 9], and thus we omit the details here. The aim of this paper is to consider the regularity criterion; we will prove the following theorem.

Theorem 1.1 Let ρ 0 W 1 , q (Ω), u 0 H 0 1 (Ω) H 2 (Ω), d 0 H 3 (Ω) with 3<q6 and ρ 0 0, div u 0 =0 in Ω and ν d 0 =0 on Ω. We also assume that the following compatibility condition holds true: ( π 0 ,g) L 2 (Ω) such that

π 0 Δ u 0 +( d 0 d 0 )= ρ 0 g in Ω.

Let (ρ,u,d) be a local strong solution to the problem (1.1)-(1.6). If u satisfies

0 T u ( t ) L q 2 q q 3 dt< with 3<q
(1.8)

and 0<T<, then the solution (ρ,u,d) can be extended beyond T>0.

Remark 1.1 When ρ1, our result improves (1.7) to (1.8).

Remark 1.2 By similar calculations as those in [6], we can replace L q -norm in (1.8) by L w q -norm, and thus we omit the details here.

Remark 1.3 When the space dimension n=2, we can prove that the problem (1.1)-(1.6) has a unique global-in-time strong solution by the same method as that in [10], and thus we omit the details here.

Next we consider another liquid model: (1.1), (1.2), (1.3), (1.5), (1.6) and

t d+udΔd= | d | 2 d,
(1.9)

with |d|1 in (0,)×Ω. Li and Wang [9] proved that the problem has a unique local strong solution. When Ω:= R 3 , Fan et al. [11] proved a regularity criterion. The aim of this paper is to study the regularity criterion of the problem in a bounded domain. We will prove the following theorem.

Theorem 1.2 Let the initial data satisfy the same conditions in Theorem  1.1 and | d 0 |1 in Ω. Let (ρ,u,d) be a local strong solution to the problem (1.1)-(1.3), (1.5), (1.6) and (1.9). If u andd satisfy

0 T ( u ( t ) L q 2 q q 3 + d L q 2 q q 3 ) dt< with 3<q
(1.10)

and 0<T<, then the solution (ρ,u,d) can be extended beyond T>0.

2 Proof of Theorem 1.1

We only need to establish a priori estimates.

Below we shall use the notation

= Ω .

First, thanks to the maximum principle, it follows from (1.1) and (1.2) that

0ρ ρ 0 L <.
(2.1)

Testing (1.3) by u and using (1.1) and (1.2), we see that

1 2 d d t ρ u 2 dx+ | u | 2 dx=(u)dΔddx.
(2.2)

Testing (1.4) by Δd+( | d | 2 1)d and using (1.1), we find that

d d t ( 1 2 | d | 2 + 1 4 ( | d | 2 1 ) 2 ) d x + ( Δ d + ( | d | 2 1 ) d ) 2 d x = ( u ) d Δ d d x .
(2.3)

Summing up (2.2) and (2.3), we have the well-known energy inequality

1 2 d d t ( ρ u 2 + | d | 2 + 1 2 ( | d | 2 1 ) 2 ) d x + ( | u | 2 + ( Δ d + ( | d | 2 1 ) d ) 2 ) d x 0 .
(2.4)

Next, we prove the following estimate:

d L ( 0 , T ; L ) max ( 1 , d 0 L ) .
(2.5)

Without loss of generality, we assume that 1 d 0 L . Multiplying (1.4) by 2d, we get

t ϕ+uϕΔϕ+2 | d | 2 ϕ=2 | d | 2 ( d 0 L 2 1 ) 2 | d | 2 0
(2.6)

with ϕ:= | d | 2 d 0 L 2 and ϕ(,0)= | d 0 | 2 d 0 L 2 0 and ν ϕ=0 on Ω×(0,). Then (2.5) follows from (2.6) by the maximum principle.

In the following calculations, we use the following Gauss-Green formula [12]:

Ω Δ f f | f | p 2 d x = 1 2 Ω | f | p 2 | f | 2 d x + 4 p 2 p 2 Ω | | f | p / 2 | 2 d x Ω | f | p 2 ( f ) f ν d S Ω | f | p 2 ( curl f × ν ) f d S
(2.7)

and the following estimate [13, 14]:

f L p ( Ω ) C f L p ( Ω ) 1 1 p f W 1 , p ( Ω ) 1 p
(2.8)

with 1<p<.

Taking ∇ to (1.4) i , we deduce that

t d i +(u) d i + ( ( | d | 2 1 ) d i ) Δ d i = j u j j d i .

Testing the above equation by | d i | p 2 d i (2p6), using (1.1), (2.7), (2.8), (2.5) and summing over i, we derive

1 p d d t Ω | d | p d x + 1 2 Ω | d | p 2 | 2 d | 2 d x + 4 p 2 p 2 Ω | | d | p / 2 | 2 d x = i Ω | d i | p 2 ( d i ) ν d i d S + i , j Ω [ u j j d i | d i | p 2 ] d i d x i Ω ( ( | d | 2 1 ) d i ) | d i | p 2 d i d x C Ω | d | p d S i , j Ω u j ( j d i | d i | p 2 d i ) d x + C Ω | d | p d x C Ω | d | p d S + C Ω | u | | d | p / 2 | | d | p / 2 | d x + C Ω | d | p d x + Ω | u | | d | p 2 | d | p 2 1 | 2 d | d x C Ω w 2 d S + C Ω | u | w | w | d x + C Ω w 2 d x + Ω | u | w | d | p 2 1 | 2 d | d x ( w : = | d | p / 2 ) C w L 2 w H 1 + C u L q w L 2 q q 2 w L 2 + C w L 2 2 + C u L q w L 2 q q 2 | d | p 2 1 | 2 d | L 2 2 p 2 p 2 | w | L 2 2 + 1 4 | d | p 2 1 | 2 d | L 2 2 + C w L 2 2 + C u L q 2 q q 3 w L 2 2 ,

which gives

d d t Ω w 2 d x + C Ω | w | 2 d x + C Ω | d | p 2 | 2 d | 2 d x C w L 2 2 + C u L q 2 q q 3 w L 2 2 .

Therefore,

d L ( 0 , T ; L p ) Cwith 2p6.
(2.9)

Testing (1.3) by u t , using (1.1), (1.2), (2.1) and (2.9), we have

1 2 d d t | u | 2 d x + ρ | u t | 2 d x = ρ u u u t d x + d d t d d : u d x 2 d t d : u d x ρ L u L q u L 2 q q 2 ρ u t L 2 + d d t d d : u d x + 2 d t L 2 d L 6 u L 3 C u L q u L 2 1 3 q u H 2 3 q ρ u t L 2 + d d t d d : u d x + C d t L 2 u L 2 1 / 2 u H 2 1 / 2 .
(2.10)

By the H 2 -regularity theory of the Stokes system, it follows from (1.3) that

u H 2 C d T Δ d L 2 + C ρ u t + ρ u u L 2 C d L 6 Δ d L 3 + C ρ u t L 2 + C u L q u L 2 q q 2 C Δ d L 3 + C ρ u t L 2 + C u L q u L 2 1 3 q u H 2 3 q 1 2 u H 2 + C Δ d L 3 + C ρ u t L 2 + C u L q q q 3 u L 2 ,

which yields

u H 2 C ρ u t L 2 +C u L q q q 3 u L 2 +C Δ d L 3 .
(2.11)

Testing (1.4) by Δ d t , using (2.5) and (2.9), we obtain

1 2 d d t | Δ d | 2 d x + | d t | 2 d x = ( ( | d | 2 1 ) d + u d ) Δ d t d x | [ ( | d | 2 d d ) + ( u d ) ] d t | d x C ( 1 + u L q Δ d L 2 q q 2 + u L 3 d L 6 ) d t L 2 C ( 1 + u L q Δ d L 2 1 3 q d H 3 3 q + u L 2 1 / 2 u H 2 1 / 2 ) d t L 2 .
(2.12)

On the other hand, by the H 3 -regularity theory of the elliptic equation, from (1.4), (2.5) and (2.9) we infer that

d H 3 C ( d L 2 + Δ d L 2 ) C ( 1 + ( t d + u d + | d | 2 d d ) L 2 ) C ( 1 + d t L 2 + u L 3 d L 6 + u L q Δ d L 2 q q 2 ) C ( 1 + d t L 2 + u L 3 + u L q Δ d L 2 1 3 q d H 3 3 q ) ,

which gives

d H 3 C ( 1 + d t L 2 + u L 3 + u L q q q 3 Δ d L 2 ) .
(2.13)

Combining (2.11) and (2.13), we have

u H 2 + d H 3 C + C ρ u t L 2 + C d t L 2 + C u L 2 + C u L q q q 3 u L 2 + C Δ d L 2 + C u L q q q 3 Δ d L 2 .
(2.14)

Putting (2.14) into (2.10) and (2.12) and summing up, we arrive at

1 2 d d t ( | u | 2 + | Δ d | 2 ) d x + ( ρ | u t | 2 + | d t | 2 ) d x d d t d d : u d x 1 4 ρ | u t | 2 d x + 1 4 | d t | 2 d x + C + C u L 2 2 + C u L q 2 q q 3 u L 2 2 + C Δ d L 2 2 + C u L q 2 q q 3 Δ d L 2 2 ,

which leads to

u L ( 0 , T ; H 1 ) C, ρ u t L 2 ( 0 , T ; L 2 ) C,
(2.15)
d L ( 0 , T ; H 2 ) + d t L 2 ( 0 , T ; H 1 ) C.
(2.16)

It follows from (2.14), (2.15) and (2.16) that

u L 2 ( 0 , T ; H 2 ) + d L 2 ( 0 , T ; H 3 ) C.
(2.17)

Taking t to (1.3), testing by u t , using (1.1), (1.2) and (2.15), we have

1 2 d d t ρ | u t | 2 d x + | u t | 2 d x | ρ u ( u t 2 + u u u t ) d x | + | ρ u t u u t d x | + 2 | d t d : u t d x | C ρ u t L 2 u L u t L 2 + C u L 6 2 u L 6 u t L 2 + C u L 6 2 Δ u L 2 u t L 6 + C ρ u t L 2 u L 6 u L 6 2 + C ρ u t L 2 u t L 6 u L 3 + C d t L 2 d L u t L 2 1 4 u t L 2 2 + C u L ρ u t L 2 2 + C u H 2 2 + C u H 2 2 ρ u t L 2 2 + C d L 2 d t L 2 2 .
(2.18)

Taking t to (1.4), testing by Δ d t , using (2.5), (2.15), (2.16) and (2.17), we arrive at

1 2 d d t | d t | 2 d x + | Δ d t | 2 d x = ( u d + | d | 2 d d ) t Δ d t d x [ u t d + u d t + ( | d | 2 d d ) t ] Δ d t d x = ( u t d ) d t d x + [ u d t + ( | d | 2 d d ) t ] Δ d t d x ( u t L 2 d L + u t L 6 Δ d L 3 ) d t L 2 + u L 6 d t L 3 Δ d t L 2 + C d t L 2 2 1 4 u t L 2 2 + 1 4 Δ d t L 2 2 + C d L 2 d t L 2 2 + C Δ d L 3 2 d t L 2 2 + C d t L 2 2 .
(2.19)

Combining (2.18) and (2.19), we have

ρ u t L ( 0 , T ; L 2 ) + u t L 2 ( 0 , T ; H 1 ) C,
(2.20)
d t L ( 0 , T ; H 1 ) + d t L 2 ( 0 , T ; H 2 ) C.
(2.21)

It follows from (1.4), (2.21) and (2.16) that

d L ( 0 , T ; H 2 ) C.
(2.22)

It follows from (2.14), (2.15), (2.20) and (2.21) that

u L ( 0 , T ; H 2 ) + d L ( 0 , T ; H 3 ) C.
(2.23)

It follows from (1.3), (2.20) and (2.23) that

u L 2 ( 0 , T ; W 2 , 6 ) C,
(2.24)

from which it follows that

u L 2 ( 0 , T ; L ) C.
(2.25)

Applying ∇ to (1.2), testing by | ρ | q 2 ρ (2q6) and using (2.25), we have

d d t ρ L q q C u L ρ L q q ,

which implies

ρ L ( 0 , T ; L q ) C,
(2.26)

and therefore

ρ t L ( 0 , T ; L q ) = u ρ L ( 0 , T ; L q ) u L ( 0 , T ; L ) ρ L ( 0 , T ; L q ) C .
(2.27)

This completes the proof.

3 Proof of Theorem 1.2

This section is devoted to the proof of Theorem 1.2. We only need to establish a priori estimates.

First, we still have (2.1) and (2.2).

Next, we easily infer that

|d|1in (0,)×Ω.
(3.1)

Testing (1.9) by Δd | d | 2 d and using (1.1) and (3.1), we find that

1 2 d d t | d | 2 dx+ | Δ d + | d | 2 d | 2 dx=(u)dΔddx.
(3.2)

Summing up (2.2) and (3.2), we have the well-known energy inequality

1 2 d d t ( ρ u 2 + | d | 2 ) dx+ ( | u | 2 + | Δ d + | d | 2 d | 2 ) dx0.
(3.3)

Taking ∇ to (1.9) i , testing by | d i | p 2 d i (2p6), using (1.1), (2.7), (2.8) and (3.1), similarly to (2.9), we deduce that

1 p d d t Ω | d | p d x + 1 2 Ω | d | p 2 | 2 d | 2 d x + 4 p 2 p 2 Ω | | d | p / 2 | 2 d x = i Ω | d i | p 2 ( d i ) ν d i d S + i , j Ω u j j d i | d i | p 2 d i d x + Ω ( | d | 2 d ) | d | p 2 d d x p 2 p 2 Ω | w | 2 d x + C w L 2 2 + C u L q 2 q q 3 w L 2 2 + Ω | d | 2 w 2 d x + C Ω | d | | 2 d | | d | p 2 1 | d | p 2 d x ( w : = | d | p / 2 ) p 2 p 2 Ω | w | 2 d x + C w L 2 2 + C u L q 2 q q 3 w L 2 2 + d L q 2 w L 2 q q 2 2 + 1 4 Ω | d | p 2 | 2 d | 2 d x 2 p 2 p 2 Ω | w | 2 d x + C w L 2 2 + C u L q 2 q q 3 w L 2 2 + C d L q 2 q q 3 w L 2 2 + 1 4 Ω | d | p 2 | 2 d | 2 d x ,

which yields

d L ( 0 , T ; L p ) + 0 T | d | 2 | 2 d | 2 dxdtC.
(3.4)

We still have (2.10) and (2.11).

Similarly to (2.12), testing (1.9) by Δ d t , using (3.1) and (3.4), we get

1 2 d d t | Δ d | 2 d x + | d t | 2 d x = ( u d | d | 2 d ) Δ d t d x = Ω ( | d | 2 d u d ) d t d x C ( 1 + u L q Δ d L 2 q q 2 + u L 3 d L 6 ) d t L 2 + C ( d L 6 3 + | d | 2 L 2 ) d t L 2 C ( 1 + u L q Δ d L 2 1 3 q d H 3 3 q + u L 2 1 / 2 u H 2 1 / 2 + | d | 2 L 2 ) d t L 2 .
(3.5)

Similarly to (2.13), we have

d H 3 C ( 1 + d t L 2 + u L 3 + u L q q q 3 Δ d L 2 + ( | d | 2 d ) L 2 ) C ( 1 + d t L 2 + u L 3 + u L q q q 3 Δ d L 2 + | d | 2 L 2 ) .
(3.6)

Combining (2.11) and (3.6), we have

u H 2 + d H 3  the right hand side of (2.14)+C | d | 2 L 2 .
(3.7)

Putting (3.7) into (3.5) and (2.10) and using the Gronwall inequality, we still have (2.15), (2.16), (2.17) and (2.18).

Similarly to (2.19), applying t to (1.9), testing by Δ d t and using (3.4), we have

1 2 d d t | d t | 2 d x + | Δ d t | 2 d x = ( u d | d | 2 d ) t Δ d t d x = ( u t d + u d t | d | 2 d t d t | d | 2 ) Δ d t d x = ( u t d ) d t d x + ( u d t | d | 2 d t d t | d | 2 ) Δ d t d x 1 4 u t L 2 2 + 1 4 Δ d t L 2 2 + C d L 2 d t L 2 2 + C Δ d L 3 2 d t L 2 2 + C d t L 2 2 .
(3.8)

Combining (2.18) and (3.8) and using the Gronwall inequality, we still obtain (2.20) and (2.21).

By similar calculations as those in (2.22)-(2.27), we still arrive at (2.22)-(2.27).

This completes the proof.