Research article

Optimal control and analysis of a stochastic SEIR epidemic model with nonlinear incidence and treatment

  • In this paper, we represented the optimal control and dynamics of a stochastic SEIR epidemic model with nonlinear incidence and treatment rate. By using the Lyapunov function method, the existence and uniqueness of the global positive solution of the model were proved. The dynamic analysis of the stochastic model was studied and we found that the model has an ergodic stationary distribution when Rs0>1. The disease was extinct when Re0<1. The optimal solution of the disease was obtained by using the stochastic control theory. The numerical simulation of our conclusion was carried out. The results showed that the disease decreased with the increase of the control variables.

    Citation: Jinji Du, Chuangliang Qin, Yuanxian Hui. Optimal control and analysis of a stochastic SEIR epidemic model with nonlinear incidence and treatment[J]. AIMS Mathematics, 2024, 9(12): 33532-33550. doi: 10.3934/math.20241600

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  • In this paper, we represented the optimal control and dynamics of a stochastic SEIR epidemic model with nonlinear incidence and treatment rate. By using the Lyapunov function method, the existence and uniqueness of the global positive solution of the model were proved. The dynamic analysis of the stochastic model was studied and we found that the model has an ergodic stationary distribution when Rs0>1. The disease was extinct when Re0<1. The optimal solution of the disease was obtained by using the stochastic control theory. The numerical simulation of our conclusion was carried out. The results showed that the disease decreased with the increase of the control variables.



    The non-isentropic Euler equations in RN in fluid dynamics with a time-dependent linear damping and Coriolis force can be expressed as follows:

    ρt+div(ρu)=0, (1.1)
    (ρu)t+div(ρuu)+ρJu+α(t)ρu+p=0, (1.2)
    St+uS=0, (1.3)

    where u=(u1,u2,,uN)T is an N-dimensional velocity field, ρ(x,t) and p(x,t)=eSργ represent density and the pressure function respectively, JT=J representing Corilis force is an anti-symmetric matrix. The damping term α(t)ρu with α(t)0 as a coefficient of friction is proportional to the momentum.

    For the special case when α(t)=0, the equations are reduced to Euler equations extended and governed by Coriolis rotational force [1,2,3,4]. The theoretical global existence of the Euler equations with rotational forces can be referred to [5,6,7]. Further studies on stability and tropical cyclones driven by this model can be referred to [8,9,10,11,12,13].

    If J=0, (1.1)–(1.3) are reduced to non-isentropic linear-damped Euler equations, which provide an important model regarding to its physical behaviours. The system can also be used to describe compressible gas dynamics through a porous material driven by a friction force [14,15,16]. Weak solutions of the damped Euler equations are shown with asymptotic and large-time behavious in [16,17,18,19]. Chow, Fan, and Yuen, in 2017, constructed the solutions of Cartesian form with J=0 in [20], which can be regarded as a special case in this article, while taking the parameter γ and 2α in [20] to be γ+1 and α respectively. For time-dependent damping, Dong and Li studied a class of analytical solutions with free-boundary [21] in 2022.

    For the case with J=0 and α(t)=0, the system (1.1)–(1.3) is reduced to the Euler equations

    ρt+div(ρu)=0, (1.4)
    (ρu)t+div(ρuu)+p=0, (1.5)
    St+uS=0. (1.6)

    There are lots of researches on Euler equations, for example, see [22,23,24,25,26]. Among all the topics, constructing analytical and exact solutions are crucial [27,28,29,30,31,32,33,34] with a common pattern of the velocity function u in linear form in many previous studies. For non-isentropic Euler equations, Barna and Mátyás presented the analytic solutions for one-dimensional Euler equations and three-dimensional Navier-Stokes equations with polytropic equation of state [34,35], which can be referred to by taking nγ and the viscosities to be zero respectively. Based on the linear form of velocity, An, Fan, and Yuen contributed with Cartesian rotational solutions to the N-dimension isentropic compressible Euler equations (1.4)–(1.6) [36] in 2015:

    u=b(t)+A(t)x, (1.7)

    where b(t) and A(t) are vector and matrix respectively. Further studies have shown the existence of general solutions in Cartesian form to isentropic Euler equations with damping and rotational forces in [20] and [37], respectively.

    Referring to the many blowup pheonomena studies [38,39,40], the global solution is still complicated to look for.

    In this article, the existence of a form of Cartesian solutions to non-isentropic Euler equations with rational force and linear damping (1.1)–(1.3) is proven by adopting mainly techniques on matrices, vectors, and curve integration. Enforcing eS=ρ and regarding velocity field u as an linear transformation of xRN, the problem is equivalent to finding the pressure function p, which leads us to a quadratic form and requirments on the matrix A and vector b. With this finding, we can construct some special exact solutions, which could be utilized in benchmarks for testings, simulations of computing flows.

    In the following sections, we will prove the existence of the non-isentropic damped Euler equations with Coriolis forces, which admit Cartesian solutions by using appropriate requirements on matrix A and vector b. We will give examples on this first cartesian form solutions to non-isentropic Euler equations based on our finding.

    In this section, we consider the non-isentropic Euler equations. Suppose that the density ρ and pressure p satisfy the relation

    p(ρ)=eSργ, (3.1)

    where the constant γ=cp/cu1, and cp and cu are the specific heats per unit mass under constant pressure and constant volume, respectively. Then we have the following theorem.

    Theorem 3.1. If matrices A with tr(A)=0 and B=(At+A2+JA+α(t)A)/2 satisfy the matrix differential equations

    BT=B, (3.2)
    Bt+BA+ATB=0, (3.3)

    then the compressible Euler equations with a time-dependent linear damping and Coriolis force (1.1)–(1.3) have explicit solutions in the form

    u=b(t)+Ax, (3.4)
    ρ=μ[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]1γ, (3.5)
    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)], (3.6)

    where μ=(γγ+1)1γ; the vector function b(t) and scalar function c(t) satisfy the ordinary differential equations:

    (bt+Ab+Jb+α(t)b)t+AT(bt+Ab+Jb+α(t)b)+2Bb=0, (3.7)
    ctbT(bt+Ab+Jb+α(t)b)=0. (3.8)

    Proof. By (3.65), (3.5) and (3.6), ρ>0, S=lnρ. Let

    ˉp=γ+1γργ, (3.9)
    pρ=1ρ(esργ)=1ρ(ργ+1)=(γ+1)ργ1ρ=(γ+1γργ)=ˉp. (3.10)

    With (3.9), the compressible Euler equations (1.2) and (1.3) can then be written as

    ρt+div(ρu)=0, (3.11)
    ut+(u)u+Ju+α(t)u+ˉp=0, (3.12)
    St+uS=0. (3.13)

    Owing to the equivalent relation (3.9) between ˉp and ρ, we mainly deal with ˉp when solving Eqs (3.11) and (3.12). Substituting Eq (3.4) into Eq (3.12), we have

    ut+(u)u+Ju+α(t)u+ˉp (3.14)
    =bt+Atx+[(b+Ax)](b+Ax)+JAx+α(t)Ax+Jb+α(t)b+ˉp (3.15)
    =bt+Jb+α(t)b+Atx+(b)Ax+(Ax)Ax+JAx+α(t)Ax+ˉp (3.16)
    =bt+(A+J+α(t))b+(At+A2+JA+α(t)A)x+ˉp=0. (3.17)

    Let

    B=(bij)N×N=12(At+A2+JA+α(t)A),     J=(gij)N×N. (3.18)

    Then the above equation can be written into a component form

    Qi(x1,,xN)bitα(t)biNk=1(aikbk+gikbk+2bikxk)=ˉpxi,      i=1,2,,N. (3.19)

    Then, the following sufficient and necessary compatible conditions of these N equations,

    Qj(x1,,xN)xi=Qi(x1,,xN)xj,      i,j=1,2,,N, (3.20)

    lead to

    bji=bij,      i,j=1,2,,N, (3.21)

    which implies that B=12(At+A2+JA+α(t)A) is a symmetric matrix. Under the condition (3.20), ˉp(x) is a complete differential function,

    dˉp(x)=Ni=1ˉp(x)xidxi=Ni=1Qi(x1,,xN)dxi. (3.22)

    Therefore we can choose a special integration route to obtain

    ˉp(x,t)=Ni=1(x1,x2,,xN)(0,0,,0)Qi(x1,x2,,xN)dxi (3.23)
    =x10Q1(x1,0,,0)dx1,+x20Q2(x1,x2,0,,0)dx2++xN0QN(x1,x2,,xN)dxN (3.24)
    =Ni=1[bi,t+Nk=1(aikbk+gikbk)+α(t)bi]xiNi=1biix2i2Ni,k=1, i<kbikxixk+c(t) (3.25)
    =xT(bt+Jb+Ab+α(t)b)xTBx+c(t). (3.26)

    Next, we show that functions (3.4)–(3.6) satisfy (3.11). By (3.9), we have

    ρt=(μˉp1γ)t=μγˉp1γ1ˉpt, (3.27)
    ρtr(A)=μˉp1γtr(A)=μγˉp1γ1γtr(A)ˉp, (3.28)
    ρ=(μˉp1γ)=μγˉp1γ1ˉp, (3.29)
    uρ=μγˉp1γ1uTˉp. (3.30)

    From Eqs (3.27)–(3.30), we have

    ρt+div(ρu)=ρt+ρtr(A)+uρ=μγˉp1γ1{xT(bt+Ab+Jb+α(t)b)t+xTBtxct(t)+γtr(A)[xT(bt+Ab+Jb+α(t)b)+xTBxc(t)]+(b+Ax)T(bt+Ab+Jb+α(t)b+2Bx)} (3.31)
    =μγˉp1γ1{xT(Bt+γtr(A)B+2ATB)x+xT[(bt+Ab+Jb+α(t)b)t+(γtr(A)I+AT)(bt+Ab+Jb+α(t)b)+2Bb][ct+γtr(A)cbT(bt+Ab+Jb+α(t)b)]} (3.32)
    =μγˉp1γ1{xT[Bt+2ATB]x+xT[(bt+Ab+Jb+α(t)b)t+AT(bt+Ab+Jb+α(t)b)+2Bb][ctbT(bt+Ab+Jb+α(t)b)]}=0, (3.33)

    where we use the condition of the first term

    xT(Bt+2ATB)x=0, (3.34)

    which is equivalent to

    (Bt+2ATB)T=(Bt+2ATB), (3.35)

    that is,

    Bt+BA+ATB=0, (3.36)

    which is (3.3). The second and third terms are controlled to be 0 with (3.7) and (3.8). By (3.6), we have

    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]=lnρ. (3.37)

    From (3.9), (3.37) is equivalent to

    S=ln(μˉpγ)=lnμ+1γlnˉp, (3.38)
    St=(lnˉp)tγ=1γˉp1ˉpt, (3.39)
    S=1γlnˉp=1γˉp1ˉp. (3.40)

    Substituting (3.4)–(3.6) and (3.38)–(3.40) to (3.13) and using (3.3), (3.7), and (3.8), we obtain by a similar argument used in obtaining Eq (3.33) that

    St+uS=1γˉp1(ˉpt+uTˉp) (3.41)
    =1γˉp1[xT(bt+Ab+Jb+α(t)b)txTBtx+ct(t)(xTAT+bT)(bt+Ab+Jb+α(t)b+2Bx)] (3.42)
    =1γˉp{xT[(bt+Ab+Jb+α(t)b)t+AT(bt+Ab+Jb+α(t)b)+2Bb]xT[Bt+2ATB]x+ct(t)bT(bt+Ab+Jb+α(t)b)}=0. (3.43)

    We observe that Eq (3.3) is a N2 matrix differential equation, which demands us to apply special reduction conditions to acquire solutions.

    Corollary 3.1. If A is an anti-symmetric matrix, that is

    AT=A, (3.44)

    and the following conditions are satisfied:

    At+α(t)A=0, (3.45)
    AJ=JA, (3.46)
    Bt=0, (3.47)
    btt+2Atb+(Jb+α(t)b)t=0, (3.48)
    ctbT(bt+Ab+Jb+α(t)b)=0, (3.49)

    then the compressible Euler equations (3.11)–(3.13) admit a general solution

    u=b(t)+Ax, (3.50)
    ρ=μ[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]1γ, (3.51)
    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]. (3.52)

    Proof. By (3.45) and (3.46),

    BT=12(At+A2+JA+α(t)A)T (3.53)
    =12[(A)(A)+(A)(J)] (3.54)
    =12(A2+JA)=B. (3.55)

    We can then simplify (3.3), (3.7), and (3.8) into (3.47), (3.48), and (3.49). Since matrix A is anti-symmetric, we have

    BA+ATB=0. (3.56)

    By (3.47), we have

    Bt=0, (3.57)
    Bt+BA+ATB=0. (3.58)

    Thus, Eq (3.3) is ensured.

    Since

    BT=B, (3.59)
    AJ=JA, (3.60)
    AT+A=0, (3.61)

    we have

    (bt+Ab+Jb+α(t)b)t+AT(bt+Ab+Jb+α(t)b)+2Bb (3.62)
    =btt+Atb+AbtAbtA(Ab+Jb+α(t)b)+(At+A2+JA+α(t)A)b+(Jb+α(t)b)t (3.63)
    =btt+2Atb+(Jb+α(t)b)t=0. (3.64)

    Thus, Eq (3.64) is simplified to (3.48).

    Next, we give the following examples in 2 to N-dimension to demonstrate special cases of this corollary.

    Remark 3.1. As (3.5) and (3.6) demand

    xT(bt+Jb+α(t)b+Ab)xTBx+c(t)>0 (3.65)

    for the positivity of the argument of the logarithm and density, the solutions exist locally.

    Example 3.1. When α=0, we have the following examples:

    2-dimensional Case: We take constant matrix

    A=J=k1[0110], b=k2[cos(k1t)sin(k1t)], c(t)=0 (3.66)

    where k1 and k2 are arbitrary constants.

    By (3.18),

    B=12(At+A2+JA+α(t)A)=12(2A2)=A2 (3.67)
    =k12[1001]. (3.68)

    Since A is a constant matrix, At=0, taking α(t)=0,

    Bt=d(At+A2+JA+α(t)A)2dt=0, (3.69)

    Eqs (3.45) and (3.47) are satisfied. As J=A, Eq (3.46) is guaranteed. Equation (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.70)
    =k12b+0+Jbt+0 (3.71)
    =k12k2[cos(k1t)sin(k1t)]+k12k2[0110][sin(k1t)cos(k1t)]=0 (3.72)

    Eq (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.73)
    =0k2[cos(k1t)sin(k1t)]T(k1k2[sin(k1t)cos(k1t)]+2k1k2[0110][cos(k1t)sin(k1t)]) (3.74)
    =k1k22[cos(k1t)sin(k1t)]T[sin(k1t)cos(k1t)]=0. (3.75)

    we obtain the following solution:

    u(t)=[k2cos(k1t)+k1x2k2sin(k1t)k1x1], (3.76)
    ρ=μ[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]1γ (3.77)
    =μ[xT(bt+2Ab)xTA2x]1γ (3.78)
    =μ[xT(k1k2[sin(k1t)cos(k1t)]+2k1k2[sin(k1t)cos(k1t)])xTk12[1001]x]1γ (3.79)
    =μ[k12(x12+x22)+k1k2(sin(k1t)x1+cos(k1t)x2)]1γ, (3.80)
    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)] (3.81)
    =lnμ+1γln[k12(x12+x22)+k1k2(sin(k1t)x1+cos(k1t)x2)]. (3.82)

    3-dimensional Case: We take constant matrix

    A=J=k1[011101110], b=k2t[111], c(t)=3k222t2 (3.83)

    where k1 and k2 are arbitrary constants.

    Since matrix A is a constant matrix, (3.45)–(3.47) are satisfied. By using of (3.83), (3.48) and (3.49) are ensured. By (3.18),

    B=12(At+A2+JA+α(t)A)=12(2A2)=A2 (3.84)
    =k12[211121112]. (3.85)

    Since A is a constant matrix, At=0, taking α(t)=0,

    Bt=d(At+A2+JA+α(t)A)2dt=0, (3.86)

    Eqs (3.45) and (3.47) are satisfied. As J=A, Eq (3.46) is guaranteed. Equation (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.87)
    =0+0+Jbt+0 (3.88)
    =k1k2[011101110][111]=0 (3.89)

    Eq (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.90)
    =3k22tk2[ttt]T(k2[111]+2k1k2[011101110][ttt]) (3.91)
    =3k22t3k22t+0=0. (3.92)

    Therefore we obtain the solution:

    u(t)=[k2t+k1(x2x3)k2t+k1(x3x1)k2t+k1(x1x2)], (3.93)
    ρ=μ[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]1γ (3.94)
    =μ[xT(bt+2Ab)xTA2x+3k222t2]1γ (3.95)
    =μ[xT(k2[111]+0)xTk12[211121112]x+3k222t2]1γ (3.96)
    =μ[2k12(x12+x22+x32x1x2x1x3x2x3)k2(x1+x2+x3)+3k222t2]1γ, (3.97)
    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)] (3.98)
    =lnμ+1γln[2k12(x12+x22+x32x1x2x1x3x2x3)k2(x1+x2+x3)+3k222t2]. (3.99)

    Remark 3.2. The 3-dimensional example has the same setting with Example 5 in [37], which admits the same u solution but has different entropy and density.

    4-dimensional Case: We take

    A=J=k1[0211201311021320], (3.100)
    b=k2t[1111], c(t)=2k22t2 (3.101)

    where k1 and k2 are arbitrary constants. By (3.18),

    B=12(At+A2+JA+α(t)A)=12(2A2)=A2 (3.102)
    =k12[624821484486284214]. (3.103)

    Since A is a constant matrix, At=0, taking α(t)=0,

    Bt=d(At+A2+JA+α(t)A)2dt=0, (3.104)

    Eqs (3.45) and (3.47) are satisfied. As J=A, Eq (3.46) is guaranteed. Equation (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.105)
    =0+0+Jbt+0 (3.106)
    =k1k2[0211201311021320][1111]=0 (3.107)

    Eq (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.108)
    =4k22tk2[tttt]T(k2[1111]+2k1k2[0211201311021320][tttt]) (3.109)
    =4k22t4k22t+0=0. (3.110)

    We have the following solutions:

    u=k2t[1111]+k1[2x2+x3+x42x1+x33x4x1x2+2x4x1+3x22x3], (3.111)
    ρ=μ[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)]1γ (3.112)
    =μ[xT(bt+2Ab)xTA2x+2k22t2]1γ (3.113)
    =μ[xT(k2[1111]+0)xTk12[624821484486284214]x+2k22t2]1γ (3.114)
    =μ[k2(x1+x2+x3+x4)+k21(6x12+14x22+6x32+14x424x1x2+8x1x316x1x416x2x38x2x44x3x4)+2k22t2]1γ, (3.115)
    S=lnμ+1γln[xT(bt+Jb+α(t)b+Ab)xTBx+c(t)] (3.116)
    =lnμ+1γln[k2(x1+x2+x3+x4)+k21(6x12+10x22+6x32+14x424x1x2+8x1x316x1x416x2x38x2x44x3x4)+2k22t2]. (3.117)

    Example 3.2. When α is a constant, we have the following examples.

    2-dimensional Case: We take

    A=J=k1eαt[0110], b=k2eαt[11],  (3.118)

    c(t)=m>0, where k1, k2, and m are arbitrary constants. Then we get a solution

    u(t)=eαt[k1x2+k2k1x1+k2], (3.119)
    ρ=μm1γ, (3.120)
    S=lnμ+1γlnm. (3.121)

    3-dimensional Case: We take

    A=J=k1eαt[011101110], b=k2eαt[111], (3.122)

    c(t)=m>0, where k1, k2, and m are arbitrary constants. Then we get a solution

    u(t)=eαt[k1(x2+x3)+k2k1(x3x1)+k2k1(x1+x2)+k2], (3.123)
    ρ=μm1γ, (3.124)
    S=lnμ+1γlnm. (3.125)

    4-dimensional Case: We take

    A=J=k1eαt[0111101111011110], b=k2eαt[1111], (3.126)

    c(t)=m>0, where k1, k2, and m are arbitrary constants. Then we get a solution

    u(t)=eαt[k1(x2+x3+x4)+k2k1(x3+x4x1)+k2k1(x4x1x2)+k2k1(x1+x2+x3)+k2], (3.127)
    ρ=μm1γ, (3.128)
    S=lnμ+1γlnm. (3.129)

    N-dimensional Case: We take

    A=k1eαt[0111101111111110]b=k2eαt[111] (3.130)
    J=A,    c(t)=m>0 (3.131)

    where k1, k2, and m are arbitrary constants. Then we get a solution

    ui=eαt[k1(Nk=i+1xki1k=1xk)+k2], (3.132)
    ρ=μm1γ, (3.133)
    S=lnμ+1γlnm. (3.134)

    Proof. Since N-dimensional case covers 2 to 4-dimensional cases, here gives the verification of N-dimensional case. (3.46) is guaranteed by J=A, with

    At=αk1eαt=αA, (3.135)

    (3.45) is satisfied. Therefore,

    B=12(At+A2+JA+αA)=0,  Bt=0, (3.136)

    (3.47) is ensured. Substituting (3.130) and (3.131) into (3.48) and (3.49) produces

    btt+2Atb+(Jb+α(t)b)t (3.137)
    =α2b+2αAb+(αbAb)t (3.138)
    =α2b+2αAbα2b2αAb=0, (3.139)

    and

    ctbT(bt+αb+Ab+Jb) (3.140)
    =0bT(αb+αbJb+Jb)=0. (3.141)

    When α(t) is not a constant, we have the following examples.

    Example 3.3. (2-dimensional case) We take

    A=tk1[0110], J=(tk1k2tk1)[0110], b=tk1[11], c(t)=βα(t)=k1t (3.142)

    where k1<0, k2, and β are arbitrary constants. As

    AJ=JA=(t2k1k2)[1001] (3.143)

    (3.46) is satisfied.

    Denoting

    Q=(qij)N×N=[0110]w=[11] (3.144)

    it is easy to see

    At=k1tk11Q=α(t)A (3.145)

    and,

    B=A2+JA2=(A+J)A2=k22tk1QA=k22I=BT (3.146)
    Bt=(k22I)t=0, (3.147)

    therefore, (3.47) is satisfied. Since

    bt=α(t)b,J=k2tk1QA (3.148)

    (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.149)
    =(α(t)b)t2α(t)Ab+[(k2tk1QA)tk1w]t+(α(t)b)t (3.150)
    =2α(t)Ab(Ab)t (3.151)
    =2α(t)AbAbtAtb (3.152)
    =2α(t)Ab+α(t)Ab+α(t)Ab=0 (3.153)

    (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.154)
    =0tk1wT[k1tk11w+tk1Qtk1w+(k2tk1tk1)Qtk1wk1tk11w] (3.155)
    =0tk1wT(k2tk1Qtk1w) (3.156)
    =k2tk1wTQw (3.157)
    =k2tk1Ni=1,j=1qij=0. (3.158)

    Then we get a solution

    u(t)=tk1[1+x21x1], (3.159)
    ρ=μ[k2(x12+x222x1x2)+β]1γ, (3.160)
    S=lnμ+1γln[k2(x12+x222x1x2)+β]. (3.161)

    Example 3.4 (3-dimensional case). We take

    A=tk1[011101110], J=(tk1k2tk1)[011101110], b=tk1[111]c(t)=βα(t)=k1t (3.162)

    where k1<0, k2, and β are arbitrary constants. As

    AJ=JA=(t2k1k2)[211121112] (3.163)

    (3.46) is satisfied.

    Denoting

    Q=(qij)N×N=[011101110]w=[111] (3.164)

    it is easy to see

    At=α(t)A (3.165)
    B=A2+JA2=(A+J)A2=k22tk1QA=k22Q2=BT (3.166)
    B=A2+JA2=k22[211121112], (3.167)

    therefore

    BT=BBt=0 (3.168)

    (3.47) is satisfied.

    Since

    bt=α(t)bJ=k2tk1QA (3.169)

    (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.170)
    =(α(t)b)t2α(t)Ab+[(k2tk1QA)tk1w]t+(α(t)b)t (3.171)
    =2α(t)Ab(Ab)t (3.172)
    =2α(t)AbAbtAtb (3.173)
    =2α(t)Ab+α(t)Ab+α(t)Ab=0 (3.174)

    (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.175)
    =0tk1wT[k1tk11w+tk1Qtk1w+(k2tk1tk1)Qtk1wk1tk11w] (3.176)
    =0tk1wT(k2tk1Qtk1w) (3.177)
    =k2tk1wTQw (3.178)
    =k2tk1Ni=1,j=1qij=0. (3.179)

    We then get a solution

    u(t)=tk1[x2+x3+1x3x1+1x1x2+1], (3.180)
    ρ=μ[k2(x12+x22+x32+x1x2+x2x3x1x32x1+2x3)+β]1γ, (3.181)
    S=lnμ+1γln[k2(x12+x22+x32+x1x2+x2x3x1x32x1+2x3)+β]. (3.182)

    Remark 3.3 (N-dimensional case). We can abtain N-dimensional solutions denoting

    Q=(qij)N×N=[0111101111111110]w=[111] (3.183)

    and taking

    A=f(t)Q, J=(k1f(t)f(t))Q, b=f(t)w, α(t)=˙f(t)f(t)c(t)=β, (3.184)

    where ˙f(t)f(t)0, k1 and β are arbitrary constants. As

    AJ=JA=(k1f(t)2)Q2, (3.185)

    (3.46) is satisfied. It is easy to see

    At=α(t)A (3.186)
    B=A2+JA2=(A+J)A2=k12f(t)Qf(t)Q=k12Q2 (3.187)

    therefore

    BT=BBt=0 (3.188)

    (3.47) are satisfied. Since

    bt=α(t)bJ=k1f(t)QA (3.189)

    (3.48) is satisfied by

    btt+2Atb+(Jb+α(t)b)t (3.190)
    =(α(t)b)t2α(t)Ab+[(k1f(t)f(t))Qf(t)w]t+(α(t)b)t (3.191)
    =2α(t)Ab+(k1QwAb)t (3.192)
    =2α(t)Ab(Ab)t (3.193)
    =2α(t)AbAbtAtb (3.194)
    =2α(t)Ab+α(t)Ab+α(t)Ab=0 (3.195)

    (3.49) is satisfied by

    ctbT(bt+Ab+Jb+α(t)b) (3.196)
    =0f(t)wT[˙f(t)w+f(t)Qf(t)w+(k1f(t)f(t))Qf(t)w˙f(t)w] (3.197)
    =0f(t)wT(k1f(t)Qf(t)w) (3.198)
    =k1f(t)wTQw (3.199)
    =k1f(t)Ni=1,j=1qij=0. (3.200)

    In this paper, we construct the Cartesian solutions

    u=b(t)+A(t)x

    for the non-isentropic Euler equations with a time-dependent linear damping and a rotational force. By constructing appropriate matices A(t) and vectors b(t), we obtain new theoretical new exact solutions, which are obtained under the requirement of entropy S=lnρ. We then invite the scientific community to provide solutions with other forms of or more general form of entropy. The global existence of the solutions remains open, while the blowup phenomena are complicated to higher dimensional cases due to the existence of many temporal variables and the multiple requirements imposed on them.

    The author declares there is no interest in relation to this article.

    Verification of examples on Euler equations

    For simplicity, we use the same ˉp defined in (3.9), solutions of ρ and S in all dimensions are equivalent to

    ρ=μˉp1γ, (4.1)
    S=lnμ+1γlnˉp. (4.2)

    It is clear that from the theorem (3.5) and (3.6) and can be easily verified from substitution that all solutions satisfy S=lnρ. Dividing ρ from both sides of (1.2), we rewrite the Euler equations (1.1)–(1.3) as

    ρt+Nk=1xkρuk=0, (4.3)
    uit+Nk=1uk(uixk+jik)+αui+γ+1γxiργ=0, (4.4)
    St+Nk=1ukxkS=0. (4.5)

    Example 1

    For 2-dimension case: Substituting (3.76)–(3.82) and (4.1) into (4.3) produces

    ρt+x1(ρu1)+x2(ρu2) (4.6)
    =μ(ˉp1γ)t+x1(μˉp1γu1)+x2(μˉp1γu2) (4.7)
    =μγˉp1γγˉpt+(k2cos(k1t)+k1x2)x1μˉp1γ+(k2cos(k1t)k1x1)x2μˉp1γ (4.8)
    =μγˉp1γγ[k21k2cos(k1t)x1k21k2sin(k1t)x2]+μγˉp1γγx1[ˉp(k2cos(k1t)+k1x2)]+μγˉp1γγx2[ˉp(k2cos(k1t)k1x1)] (4.9)
    =μγˉp1γγ{k21k2cos(k1t)x1k21k2sin(k1t)x2+x1[k12(x12+x22)+k1k2(sin(k1t)x1+cos(k1t)x2)](k2cos(k1t)+k1x2)+x2[k12(x12+x22)+k1k2(sin(k1t)x1+cos(k1t)x2)](k2sin(k1t)k1x1)} (4.10)
    =μγˉp1γγ[k21k2cos(k1t)x1k21k2sin(k1t)x2+(2k21x1k1k2sin(k1t))(k2cos(k1t)+k1x2)+(2k21x2+k1k2cos(k1t))(k2sin(k1t)k1x1)]=0. (4.11)

    Substituting (3.76)–(3.82) into (4.4), the first momentum gives

    u1t+u1(u1x1+j11)+u2(u1x2+j12)+αu1+γ+1γx1ργ (4.12)
    =k1k2sin(k1t)+u1(0+0)+(k2sin(k1t)k1x1)(k1+k1)+2k21x1k1k2sin(k1t) (4.13)
    =0, (4.14)

    the second momentum gives

    u2t+u1(u2x1+j11)+u2(u2x2+j12)+αu2+γ+1γx2ργ (4.15)
    =k1k2sin(k1t)+(k2cos(k1t)k1x2)(k1k1)+u2(0+0)+2k21x2k1k2cos(k1t) (4.16)
    =0. (4.17)

    Substituting (3.76)–(3.82) into (4.5) gives

    St+u1x1S+u2x2S (4.18)
    =1γˉp(k21k2cos(k1t)x1k21k2sin(k1t)x2)+1γˉp(2k21x1k1k2sin(k1t))(k2cos(k1t)+k1x2)+1γˉp(2k21x2+k1k2cos(k1t))(k2sin(k1t)k1x1) (4.19)
    =1γˉp(k21k2cos(k1t)x1k21k2sin(k1t)x2)+1γˉp(k21k2sin(k1t)x2+k21k2cos(k1t)x1)=0. (4.20)

    For 3-dimensional case: Substituting (3.93)–(3.99) and (4.1) into (4.3) produces

    ρt+x1(ρu1)+x2(ρu2)+x3(ρu3) (4.21)
    =μ(ˉp1γ)t+x1(μˉp1γu1)+x2(μˉp1γu2)+x3(μˉp1γu3) (4.22)
    =μγˉp1γγˉpt+[k2t+k1(x2x3)]x1μˉp1γ+[k2t+k1(x3x1)]x2μˉp1γ+[k2t+k1(x1x2)]x3μˉp1γ (4.23)
    =μγˉp1γγ3k22t+μγˉp1γγ[k2t+k1(x2x3)]ˉpx1+μγˉp1γγ[k2t+k1(x3x1)]ˉpx2+μγˉp1γγ[k2t+k1(x1x2)]ˉpx3 (4.24)
    =μγˉp1γγ{3k22t+[k2t+k1(x2x3)]ˉpx1+[k2t+k1(x3x1)]ˉpx2+[k2t+k1(x1x2)]ˉpx3} (4.25)
    =μγˉp1γγ{3k22t+[k2t+k1(x2x3)][2k22(2x1x2x3)k2]+[k2t+k1(x3x1)][2k22(2x2x1x3)k2]+[k2t+k1(x1x2)][2k22(2x3x1x2)k2]}=0. (4.26)

    Substituting (3.93)–(3.99) into (4.4), the first momentum gives

    u1t+u1(u1x1+j11)+u2(u1x2+j12)+u3(u1x3+j13)+αu1+γ+1γx1ργ (4.27)
    =k2+u1(0+0)+[k2t+k1(x3x1)](k1+k1)+[k2t+k1(x1x2)](k1k1)+2k21(2x1x2x3)k2=0, (4.28)

    the second momentum gives

    u2t+u1(u2x1+j21)+u2(u2x2+j22)+u3(u2x3+j23)+αu2+γ+1γx2ργ (4.29)
    =k2+[k2t+k1(x2x3)](k1k1)+u2(0+0)+[k2t+k1(x1x2)](k1+k1)+2k21(2x2x1x3)k2=0, (4.30)

    the third momentum gives

    u3t+u1(u3x1+j31)+u2(u3x2+j32)+u3(u3x3+j33)+αu3+γ+1γx3ργ (4.31)
    =k2+[k2t+k1(x2x3)](k1+k1)+[k2t+k1(x3x1)](k1k1)+u3(0+0)+2k21(2x3x1x2)k2=0. (4.32)

    Substituting (3.93)–(3.99) into (4.5) gives

    St+u1x1S+u2x2S+u3x3S (4.33)
    =1γˉp3k22t+[k2t+k1(x2x3)]x1lnˉp+[k2t+k1(x3x1)]x2lnˉp+[k2t+k1(x1x2)]x3lnˉp (4.34)
    =1γˉp{3k22t+[k2t+k1(x2x3)][2k21(2x1x2x3)k2]+[k2t+k1(x3x1)][2k21(2x2x1x3)k2]+[k2t+k1(x1x2)][2k21(2x3x1x2)k2]}=0. (4.35)

    For 4-dimensional case: Substituting (3.111)–(3.117) and (4.1) into (4.3) produces

    ρt+x1(ρu1)+x2(ρu2)+x3(ρu3)+x4(ρu4) (4.36)
    =μ(ˉp1γ)t+x1(μˉp1γu1)+x2(μˉp1γu2)+x3(μˉp1γu3)+x4(μˉp1γu4) (4.37)
    =μγˉp1γγˉpt+[k2t+k1(2x2+x3+x4)]x1μˉp1γ+[k2t+k1(2x1+x33x4)]x2μˉp1γ+[k2t+k1(x1x2+2x4)]x3μˉp1γ+[k2t+k1(x1+3x22x3)]x4μˉp1γ (4.38)
    =μγˉp1γγ4k22t+μγˉp1γγ[k2t+k1(2x2+x3+x4)]ˉpx1+μγˉp1γγ[k2t+k1(2x1+x33x4)]ˉpx2+μγˉp1γγ[k2t+k1(x1x2+2x4)]ˉpx3+μγˉp1γγ[k2t+k1(x1+3x22x3)]ˉpx4 (4.39)
    =μγˉp1γγ{4k22t+[k2t+k1(2x2+x3+x4)]ˉpx1+[k2t+k1(2x1+x33x4)]ˉpx2+[k2t+k1(x1x2+2x4)]ˉpx3+[k2t+k1(x1+3x22x3)]ˉpx4} (4.40)
    =μγˉp1γγ{4k22t+[k2t+k1(2x2+x3+x4)][k2+k21(12x14x2+8x316x4)]+[k2t+k1(2x1+x33x4)][k2+k21(28x24x116x38x4)]+[k2t+k1(x1x2+2x4)][k2+k21(12x3+8x116x24x4)]+[k2t+k1(x1+3x22x3)][k2+k21(28x416x18x24x3)]}=0. (4.41)

    Substituting (3.111)–(3.117) into (4.4), the first momentum gives

    u1t+u1(u1x1+j11)+u2(u1x2+j12)+u3(u1x3+j13)+u4(u1x4+j14)+αu1+γ+1γx1ργ (4.42)
    =k2+u1(0+0)+[k2t+k1(2x1+x33x4)](2k12k1)+[k2t+k1(x1x2+2x4)](k1+k1)+[k2t+k1(x1+3x22x3)](k1+k1)k2+k21(12x14x2+8x316x4)=0, (4.43)

    the second momentum gives

    u2t+u1(u2x1+j21)+u2(u2x2+j22)+u3(u2x3+j23)+u4(u2x4+j24)+αu2+γ+1γx2ργ (4.44)
    =k2+[k2t+k1(2x2+x3+x4)](2k1+2k1)+u2(0+0)+[k2t+k1(x1x2+2x4)](k1+k1)+[k2t+k1(x1+3x22x3)](3k13k1)k2+k21(4x1+28x216x38x4)=0, (4.45)

    the third momentum gives

    u3t+u1(u3x1+j31)+u2(u3x2+j32)+u3(u3x3+j33)+u4(u3x4+j34)+αu3+γ+1γx3ργ (4.46)
    =k2+[k2t+k1(2x2+x3+x4)](k1k1)+[k2t+k1(2x1+x33x4)](k1k1)+u3(0+0)+[k2t+k1(x1+3x22x3)](2k1+2k1)k2+k21(8x116x2+12x34x4)=0, (4.47)

    the fourth momentum gives

    u4t+u1(u4x1+j41)+u2(u4x2+j42)+u3(u4x3+j43)+u4(u4x4+j44)+αu4+γ+1γx4ργ (4.48)
    =k2+[k2t+k1(2x2+x3+x4)](k1k1)+[k2t+k1(2x1+x33x4)](3k1+3k1)+[k2t+k1(x1x2+2x4)](2k12k1)+u4(0+0)k2+k21(16x18x24x3+28x4)=0. (4.49)

    Substituting (3.111)–(3.117) into (4.5) gives

    St+u1x1S+u2x2S+u3x3S+u4x4S (4.50)
    =ˉptγˉp+u1x1lnˉpγ+u2x2lnˉpγ+u3x3lnˉpγ+u4x4lnˉpγ (4.51)
    =1γˉp{4k22t+[k2t+k1(2x2+x3+x4)][k2+k21(12x14x2+8x316x4)]+[k2t+k1(2x1+x33x4)][k2+k21(28x24x116x38x4)]+[k2t+k1(x1x2+2x4)][k2+k21(12x3+8x116x24x4)]+[k2t+k1(x1+3x22x3)][k2+k21(28x416x18x24x3)]}=0. (4.52)

    Example 2

    Since N-dimensional case covers 2 to 4-dimensional cases, here gives the verification of N-dimensional case. Substituting solutions into Euler equations, as S is a constant, (4.5) is guaranteed. Since ρ is also a constant, by

    ρt+Nk=1xkρuk (4.53)
    =0+ρNk=1xkuk (4.54)
    =ρeαtNk=1xk[k1(Ng=k+1xgk1g=1xg)+k2]=0, (4.55)

    Eq (4.3) is verified.

    uixk=xkeαt[k1(Nk=i+1xki1k=1xk)+k2] (4.56)
    ={k1eαt,for k<i0,for k=ik1eαt,for k>i}=jik, (4.57)

    therefore,

    uit+Nk=1uk(uixk+jik)+αui+γ+1γxiργ (4.58)
    =αui+0+αui+0=0, (4.59)

    the n-th momentum Eq (4.4) is satisfied.

    Example 3

    Substituting (3.159)–(3.161) into (4.3) produces

    ρt+x1ρu1+x2ρu2 (4.60)
    =0+μγˉp1γγtk1(1+x2)k2(x11)+μγˉp1γγtk1(1x1)k2(x2+1)=0. (4.61)

    Substituting (3.159)–(3.161) into (4.4) gives

    uit+u1(uixk+ji1)+u2(uixk+ji2)+αui+γ+1γxiργ (4.62)
    =u1(uixk+ji1)+u2(uixk+ji2)+0 (4.63)
    =k1tk11[1+x11x2]+tk1(1+x2)(tk1[01]+[0tk1k2tk1])+tk1(1x1)(tk1[10]+[tk1+k2tk10])k1ttk1[1+x11x2]+[k2(x11)k2(x2+1)]=0. (4.64)

    Substituting (3.159)–(3.161) into (4.5) gives

    St+u1x1S+u2x2S (4.65)
    =0+tk1(1+x2)k2(2x11)γˉp+tk1(1x1)k2(2x2+1)γˉp=0. (4.66)

    Example 4

    Substituting (3.180)–(3.182) into (4.3) produces

    ρt+x1ρu1+x2ρu2+x3ρu3 (4.67)
    =0+μγˉp1γγ[tk1(x2+x3+1)k2(2x1+x2x32)+tk1(x3x1+1)k2(2x2+x1+x3)+tk1(x1x2+1)k2(2x3x1+x2+2)]=0. (4.68)

    Substituting (3.180)–(3.182) into (4.4), since

    ut=k1tk11=k1ttk1=α(t)u, (4.69)

    we have

    uit+Nk=1uk(uixk+jik)+αui+γ+1γxiργ (4.70)
    =u1(uixk+ji1)+u2(uixk+ji2)+u3(uixk+ji3)+0 (4.71)
    =tk1(x2+x3+1)(tk1[011]+[0tk1k2tk1tk1k2tk1])+tk1(x3x1+1)(tk1[101]+[tk1+k2tk10tk1k2tk1])+tk1(x1x2+1)(tk1[110]+[tk1+k2tk1tk1+k2tk10]+[k2(2x1+x2x32)k2(2x2+x1+x3)k2(2x3x1+x22)])=0. (4.72)

    Substituting (3.180)–(3.182) into (4.5) gives

    St+u1x1S+u2x2S+u3x3S (4.73)
    =0+1γˉp[tk1(x2+x3+1)k2(2x1+x2x32)+tk1(x3x1+1)k2(2x2+x1+x3)+tk1(x1x2+1)k2(2x3x1+x2+2)]=0. (4.74)


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