Trunking Logistics for an E-grocer during Growth-A cost-centered approach in relation to service and centralization

Hospital planning process redesign from a customer-centric perspective; Herontwerp van een ziekenhuis planning proces, vanuit een klant-gericht perspectief

Hospital planning process redesign from a customer-centric perspective - Herontwerp van een ziekenhuis planning proces, vanuit een klant-gericht perspectief

IoT and Big Data in Transport Systems - Het IoT en Big Data in ransportsystemen

Enhancement of aircraft cabin comfort studies by coupling of models for human thermoregulation, internal radiation, and turbulent flows

Scientific enhancement of the analysis of thermal comfort aspects in aircraft cabins is the subject of the current investigation. For this purpose, three important processes are identified that play a significant role in thermal comfort, viz. the human response to its thermal environment which is also known as thermoregulation, the actual...

A Simple, Robust and Fast Algorithm to Compute Deformations of Multi-Block Structured Grids

A grid deformation method has been developed for the movement of multiblock, structured grids due to surface deformation arising from aeroelastics or design optimisation. The method uses a volume spline interpolation technique to compute the deformation of block vertices and block edges. After that, the deformation of block-faces is computed by...

Numerical evaluation of an effective roe scheme and chemical models for chemically reacting nozzle flows in thermal equilibrium

Numerical evaluation of an efficient roe-type flux difference scheme for thermochemical non-equilibrium nozzle flows

Numerical evaluation of an efficient ROE scheme and chemical models for chemically reacting nozzle flows in thermal equilibrium

An efficient Roe-type flux-difference scheme for chemically reacting inviscid compressible flow in thermal equilibrium is presented. The numerical scheme is validated. Three well known chemical models are compared. The set of testcases concerned quasi one-dimensional hypersonic nozzle flows, with and without strong normal Shockwaves.

Multigrid solution of the steady euler equations