共查询到20条相似文献,搜索用时 218 毫秒
1.
周叮 《应用数学和力学(英文版)》1996,17(8):773-779
ANANALYTICALSOLUTIONOFTRANSVERSEVIBRATIONOFRECTANGULARPLATESSIMPLYSUPPORTEDATTWOOPPOSITEEDGESWITHARBITRARYNUMBEROFELASTICLINE... 相似文献
2.
FORCEDOSCILLATIONSOFBOUNDARYVALUEPROBLEMSOFHIGHERORDERFUNCTIONALPARTIALDIFFERENTIALEQUATIONSJinMingZhong(靳明忠),DongYing(董莹),Li... 相似文献
3.
THEEXISTENCEOFPERIODICSOLUTIONOFTHEFOURTHORDINARYNONLINEARDIFFERENTIALEQUATIONCAUSEDBYFLOW-INDUCEDVIBRATIONGuQing-fang(顾清芳)Ta... 相似文献
4.
张祥 《应用数学和力学(英文版)》1994,(3)
SINGULARPERTURBATIONOFINITIALBOUNDARYVALUEFROBLEMSOFREACTIONDIFFUSlONEQUATIONWITHDELAYZhangXiang(张祥)(AnhuiNormalUniversity)Wu... 相似文献
5.
高永馨 《应用数学和力学(英文版)》1996,(6)
EXISTENCEOFSOLUTIONSOFTHREE-POINTBOUNDARYVALUEPROBLEMSFORNONLINEARFOURTHORDERDIFFERENTIALEQUATION¥GaoYongxin(高永馨)(Departmento... 相似文献
6.
王凡彬 《应用数学和力学(英文版)》1996,17(11):1101-1106
BLOW-UPANDDIE-OUTOFSOLUTIONSOFNONLINEARPSEUDOHYPERBOLICEQUATIONSOFGENERALIZEDNERVECONDUCTIONTYPEWangFanbin(王凡彬)(ReceivedJune2... 相似文献
7.
UNCONDITIONAL STABLE SOLUTIONS OF THE EULER EQUATIONS FOR TWO-AND THREE-D WINGS IN ARBITRARY MOTION 总被引:2,自引:0,他引:2
高正红 《应用数学和力学(英文版)》1995,16(12):1209-1220
UNCONDITIONALSTABLESOLUTIONSOFTHEEULEREQUATIONSFORTWO-ANDTHREE-DWINGSINARBITRARYMOTIONGaoZhenghong(高正红)(ReceivedJan.12,1995,C... 相似文献
8.
NUMERICALSIMULATIONOFTHREEDIMENSIONALTURBULENTFLOWINSUDDENLYEXPANDEDRECTANGULARDUCTNUMERICALSIMULATIONOFTHREEDIMENSIONALTURBU... 相似文献
9.
刘汉池 《应用数学和力学(英文版)》1995,(8)
STRESS-STBAINFIELDNEARCRACKTIPANDCALCULATIONOFCRITICALSTRESSOFCRACKPROPAGATIONINAPUREBENDINGBEAMOFRECTANGULARSECTIONWITHONE-S... 相似文献
10.
杨作东 《应用数学和力学(英文版)》1996,17(5):465-476
EXISTENCEOFPOSITIVESOLUTIONSFORACLASSOFSINGULARTWOPOINTBOUNDARYVALUEPROBLEMSOFSECONDORDERNONLINEAREQUATION(杨作东)EXISTENCEOFPOS... 相似文献
11.
Singular perturbation of boundary value problem for a vector fourth order nonlinear differential equation 总被引:1,自引:0,他引:1
We study the vector boundary value problem with boundary perturbations: ε~2y~((4))=f(x,y,y″,ε, μ) ( μ<χ<1-μ) y(χ,ε,μ)l_(χ-μ)= A_1(ε,μ), y(χ,ε,μ)l_(χ-1-μ)=B_1(ε,μ) y″(χ,ε,μ)l_(χ-μ)=A_2(ε,μ),y″(χ,ε,μ)l_(χ-1-μ)=B_2(ε,μ)where yf, A_j and B_j (j=1,2) are n-dimensional vector functions and ε,μ are two small positive parameters. This vector boundary value problem does not appear to have been studied, although the scalar boundary value problem has been treated. Under appropriate assumptions, using the method of differential inequalities we find a solution of the vector boundary value problem and obtain the uniformly valid asymptotic expansions. 相似文献
12.
We find conditions for the unique solvability of the problem u
xy
(x, y) = f(x, y, u(x, y), (D
0
r
u)(x, y)), u(x, 0) = u(0, y) = 0, x ∈ [0, a], y ∈ [0, b], where (D
0
r
u)(x, y) is the mixed Riemann-Liouville derivative of order r = (r
1, r
2), 0 < r
1, r
2 < 1, in the class of functions that have the continuous derivatives u
xy
(x, y) and (D
0
r
u)(x, y). We propose a numerical method for solving this problem and prove the convergence of the method.
__________
Translated from Neliniini Kolyvannya, Vol. 8, No. 4, pp. 456–467, October–December, 2005. 相似文献
13.
J. B. Diaz 《Archive for Rational Mechanics and Analysis》1957,1(1):357-390
This paper develops, with an eye on the numerical applications, an analogue of the classical Euler-Cauchy polygon method (which is used in the solution of the ordinary differential equation dy/dx=f(x, y), y(x
0)=y
0) for the solution of the following characteristic boundary value problem for a hyperbolic partial differential equation u
xy
=f(x, y, u, u
x
, y
y
), u(x, y
0)=(x), u(x
0, y)=(y), where (x
0)=(y
0). The method presented here, which may be roughly described as a process of bilinear interpolation, has the advantage over previously proposed methods that only the tabulated values of the given functions (x) and (y) are required for its numerical application. Particular attention is devoted to the proof that a certain sequence of approximating functions, constructed in a specified way, actually converges to a solution of the boundary value problem under consideration. Known existence theorems are thus proved by a process which can actually be employed in numerical computation.
相似文献
相似文献
14.
In this paper we study the singularly perturbed boundary value problem:εy″=f(t,y,ε),y(0)=ξ(ε),y(1)=η(ε).where εis a positive small parameter.In the conditions:f_(?)(0,y,0)≥m_0 ,f_(?)(l,y,0)≥m_0 and f_(?)f(t,y,ε)≥0 ,we prove the existences,and uniformly valid asymptotic expansions of solutions for the given boundary value problems,and hence we improve the existing results. 相似文献
15.
王洪纲 《应用数学和力学(英文版)》1982,3(5):675-681
In some investigations on variational principle for coupled thermoelastic problems, the free energy Φ(eij,θ) ,where the state variables are elastic strain eij and temperature increment θ, is expressed as Φ(eij,θ)=λ/2ekkeij=uek1ek1-γekkθ-c/2 p θ2/T0(0.1) This expression is employed only under the condition of |θ|≤T0(absolute temperature of reference) But the value of temperature increment is great, even greater than T0 in thermal shock. And the material properties (λ ,μ ,ν ,c , etc.) will not remain constant, they vary with θ. The expression of free energy for this condition.is derived in this paper. Equation (0.1) is its special case.Euler’s equations will be nonlinear while this expression of free energy has been introduced into variational theorem. In order to linearise, the time interval of thermal shock is divided into a number of time elements Δtk, (Δtk=tk-tk-1,k=1,2…,n), which are so small that the temperature increment θk within it is very small, too. Thus, the material properties may be defined by temperature field Tk-1=T(x1,x2,x3,tk-1) at instant tk-1 , and the free energy Φk expressed by eg. (0.1) may be employed in element Δtk.Hence the variational theorem will be expressed partly and approximately. 相似文献
16.
S. H. Saker 《Nonlinear Oscillations》2011,13(3):407-428
Our aim is to establish some sufficient conditions for the oscillation of the second-order quasilinear neutral functional
dynamic equation
( p(t)( [ y(t) + r(t)y( t(t) ) ]D )g )D + f( t,y( d(t) ) = 0, t ? [ t0,¥ )\mathbbT, {\left( {p(t){{\left( {{{\left[ {y(t) + r(t)y\left( {\tau (t)} \right)} \right]}^\Delta }} \right)}^\gamma }} \right)^\Delta } + f\left( {t,y\left( {\delta (t)} \right)} \right. = 0,\quad t \in {\left[ {{t_0},\infty } \right)_\mathbb{T}}, 相似文献
17.
Alexander Mielke 《Journal of Dynamics and Differential Equations》1992,4(3):419-443
We consider the equation a(y)uxx+divy(b(y)yu)+c(y)u=g(y, u) in the cylinder (–l,l)×, being elliptic where b(y)>0 and hyperbolic where b(y)<0. We construct self-adjoint realizations in L2() of the operatorAu= (1/a) divy(byu)+(c/a) in the case ofb changing sign. This leads to the abstract problem uxx+Au=g(u), whereA has a spectrum extending to + as well as to –. For l= it is shown that all sufficiently small solutions lie on an infinite-dimensional center manifold and behave like those of a hyperbolic problem. Anx-independent cross-sectional integral E=E(u, ux) is derived showing that all solutions on the center manifold remain bounded forx ±. For finitel, all small solutionsu are close to a solution on the center manifold such that u(x)-(x)
Ce
-(1-|x|) for allx, whereC and are independent ofu. Hence, the solutions are dominated by hyperbolic properties, except close to the terminal ends {±1}×, where boundary layers of elliptic type appear. 相似文献
18.
A closed-form model for the computation of temperature distribution in an infinitely extended isotropic body with a time-dependent
moving-heat sources is discussed. The temperature solutions are presented for the sources of the forms: (i) 01(t)=0
exp(−λt), (ii) 02(t) =0(t/t
*)exp(−λt), and 03(t)=0[1+a
cos(ωt)], where λ and ω are real parameters and t
* characterizes the limiting time. The reduced (or dimensionless) temperature solutions are presented in terms of the generalized
representation of an incomplete gamma function Γ(α,x;b) and its decomposition C
Γ and S
Γ. The solutions are presented for moving, -point, -line, and -plane heat sources. It is also demonstrated that the present
analysis covers the classical temperature solutions of a constant strength source under quasi-steady state situations.
Received on 13 June 1997 相似文献
19.
Skew product semiflowΠ t :X ×Y → X × Y generated by $$\left\{ \begin{gathered} u_t = u_{xx} + f(y \cdot t,x,u,u_x ), t > 0 x \in (0,1), y \in Y, \hfill \\ D or N boundary conditions \hfill \\ \end{gathered} \right.$$ is considered, whereX is an appropriate subspace ofH 2(0, 1), (Y, ?) is a compact minimal flow. By analyzing the zero crossing number for certain invariant manifolds and the linearized spectrum, it is shown that a minimal setE?X × Y ofΠ, is uniquely ergodic if and only if (Y, ?) is uniquely ergodic andμ(Y 0)=1, whereμ is the unique ergodic measure of (Y, ?),Y 0={ity∈Y} Card(E∩P ?1(y))=1},P:X × Y → Y is the natural projection (it was proved in an authors' earlier paper thatY 0 is a residual subset ofY). Moreover, if (E, ?) is uniquely ergodic, then it is topologically conjugated to a subflow ofR 1 ×Y. A consequence of the last result is the following: in the case that (Y, ?) is almost periodic,Π, is expected to have many purely almost automorphic motions which are not ergodic. 相似文献
20.
《International Journal of Solids and Structures》2003,40(2):251-269
The constitutive postulations for mixed-hardening elastoplasticity are selected. Several homeomorphisms of irreversibility parameters are derived, among which Xa0 and Xc0 play respectively the roles of temporal components of the Minkowski and conformal spacetimes. An augmented vector Xa:=(YQat,YQa0)t is constructed, whose governing equations in the plastic phase are found to be a linear system with a suitable rescaling proper time. The underlying structure of mixed-hardening elastoplasticity is a Minkowski spacetime on which the proper orthochronous Lorentz group SOo(n,1) left acts. Then, constructed is a Poincaré group ISOo(n,1) on space X:=Xa+Xb, of which Xb reflects the kinematic hardening rule in the model. We also find that the space (Qat,q0a) is a Robertson–Walker spacetime, which is conformal to Xa through a factor Y, and conformal to Xc:=(ρQat,ρQa0)t through a factor ρ as given by ρ(q0a)=Y(q0a)/[1−2ρ0Qa0(0)+2ρ0Y(q0a)Qa0(q0a)]. In the conformal spacetime the internal symmetry is a conformal group. 相似文献
|