About: Finite difference method is a research topic. Over the lifetime, 21603 publications have been published within this topic receiving 468852 citations. The topic is also known as: Finite-difference methods & FDM.
TL;DR: In this paper, the aerodynamic response of a cascade of airfoils subjected to entropic, vortical, and acoustic gusts is analyzed by linearizing the full time-dependent mass, momentum, and energy conservation equations about a nonlinear, isentropic and irrotational mean or steady flow.
Abstract: The linearized unsteady aerodynamic response of a cascade of airfoils subjected to entropic, vortical, and acoustic gusts is analyzed. Field equations for the first-order unsteady perturbation flow are obtained by linearizing the full time-dependent mass, momentum, and energy conservation equations about a nonlinear, isentropic, and irrotational mean or steady flow. A splitting technique is then used to decompose the unsteady velocity field into irrotational and rotational parts leading to field equations for the unsteady entropy, rotational velocity, and irrotational velocity fluctuations that are coupled only sequentially. The entropic and rotational velocity fluctuations can be described in terms of the mean-flow drift and stream functions which can be computed numerically. The irrotational unsteady velocity is described by an inhomogeneous linearized potential equation which contains a source term that depends on the rotational velocity field. This equation is solved via a finite difference technique. Results are presented to indicate the status of the numerical solution procedure and to demonstrate the impact of blade geometry and mean blade loading on the aerodynamic response of cascades to vortical gust excitations. The analysis described leads to very efficient predictions of cascade unsteady aerodynamics phenomena making it useful for turbomachinery aeroelastic and aeroacoustic design applications.
TL;DR: In this paper, the problem of free convection along a vertical plane source or sink with uniform lateral mass flux in a porous medium is solved by the local non-similarity approximation.
TL;DR: In this paper, an optimized, collocated-grid finite-difference scheme was proposed to solve the anisotropic velocity-stress equation in spherical coordinates by using a non-uniform grid to discretize the computational domain.
Abstract: SUMMARY
To simulate seismic wave propagation in the spherical Earth, the Earth’s curvature has to be taken into account. This can be done by solving the seismic wave equation in spherical coordinates by numerical methods. In this paper, we use an optimized, collocated-grid finite-difference scheme to solve the anisotropic velocity–stress equation in spherical coordinates. To increase the efficiency of the finite-difference algorithm, we use a non-uniform grid to discretize the computational domain. The grid varies continuously with smaller spacing in low velocity layers and thin layer regions and with larger spacing otherwise. We use stress-image setting to implement the free surface boundary condition on the stress components. To implement the free surface boundary condition on the velocity components, we use a compact scheme near the surface. If strong velocity gradient exists near the surface, a lower-order scheme is used to calculate velocity difference to stabilize the calculation. The computational domain is surrounded by complex-frequency shifted perfectly matched layers implemented through auxiliary differential equations (ADE CFS-PML) in a local Cartesian coordinate. We compare the simulation results with the results from the normal mode method in the isotropic and anisotropic models and verify the accuracy of the finite-difference method.
TL;DR: In this article, the thermally induced vibrations of functionally graded material (FGM) beams are analyzed under the assumption of uncoupled thermoelasticity laws, first order beam theory, and the von Karman type geometrical nonlinearity.
Abstract: Geometrically non-linear thermally induced vibrations of functionally graded material (FGM) beams are analyzed in this research. All thermomechanical properties of the beam are assumed to be temperature and position dependent. Beam is subjected to thermal shock on the ceramic-rich surface whereas the metal-rich one is kept at reference temperature or thermally insulated. The one-dimensional transient heat conduction equation is established and solved via a hybrid iterative central finite difference method and Crank–Nicolson method. Total functional of the beam is obtained under the assumptions of uncoupled thermoelasticity laws, first order beam theory, and the von Karman type geometrical non-linearity. The conventional multi-term p-Ritz method appropriate for arbitrary in-plane and out-of-plane boundary conditions is applied to the total functional of the system which results in the matrix representation of the equations of motion. Non-linear coupled equations of motion are solved via the iterative Newton–Raphson method accompanied with the β-Newmark time approximation technique. Numerical results are well validated with the available results for the case of isotropic homogeneous beams. Some parametric studies are conducted to examine the influences of beam geometry, material composition, temperature dependency, in-plane and out-of-plane mechanical and thermal boundary conditions. It is shown that, thermally induced vibrations indeed exist especially for the case of sufficiently thin beams.
TL;DR: In this paper, a finite difference scheme of the Crank-Nicholson type was developed by introducing an intermediate function for the heat transport equation at the microscale, which is shown by the discrete energy method that the scheme is unconditionally stable.