two-dimensional euler equations have been solved on an unstructured grid. an upwind finite volume scheme, based on roes flux difference splitting method, is used to discretize the equations. using advancing front method, an initial delaunay triangulation has been made. the adaptation procedure involves mesh enrichment coarsening in regions of flow with high low gradients of flow properties, acc...

We propose a method to compute the $R$-matrix $R$ on tensor product of Fock modules from coproduct relations in Hopf algebra. apply this quantum toroidal algebra $U_{q,t}(\overset{..}{gl}_1)$ for which is currently not explicitly known. show that reduce single elegant equation $R$. Using theory symmetric Macdonald polynomials we provides recursive formula matrix elements

In this paper, a novel control method for photovoltaic converter connection to the national gridis presented, so in addition to the injection control by solar arrays to the grid, this method cancompensate reactive power and harmonics in the load current. The system will be connected inparallel between the grid and load. The proposed system supplies all load power consumption(including active po...

Some of the simulation work performed by the computational aerosciences project under the NASA Constellation program is presented. The challenges of simulating the powered flight of the Orion launch abort vehicle for the purposes of building an aerodynamics database are discussed. During an abort this vehicle fires both a four-nozzle abort motor together with an eight-nozzle attitude control mo...

Performance of a simplified Quad Tiltrotor (QTR) is studied in ground effect using CFD. The rotor systems are modeled in a time averaged sense using source terms for the forces in the momentum equations. Viscous body conforming overset meshes are used to model all the solid surfaces of the vehicle. The background Cartesian grid is used to specify the far-field boundary conditions and transfer i...

This work couples a computational fluid dynamics (CFD) code and rotorcraft computational structural dynamics (CSD) code to calculate helicopter rotor airloads across a range of flight conditions. An iterative loose (weak) coupling methodology is used to couple the CFD and CSD codes on a per revolution, periodic basis. The CFD uses a high fidelity, Navier-Stokes, overset grid methodology with fi...

Abstract The extreme motions created a negative effect on planing hull. Otherwise, interceptors enable the improvement of hydrodynamic characteristics highspeed craft. total drag ship can be divided into two components: pressure and shear forces. This project specifically aims to predict component based CFD simulation with without an interceptor resistance components. volume fluid is used in co...