In this paper the capabilities of an automated CFD system which is currently available at NLR are demonstrated. Transonic flow around the AS28G wing/body configuration and hypersonic flow through a generic three-dimensional mixed-compression airbreathing inlet are simulated. An assessment of the level of automation of the current CFD-system is made. The problem-turnaround time lies within the order of a week for both applications.
Demonstration of an Automated CFD System for Three-Dimensional Flow Simulations
1995
18 pages
Report
No indication
English
Aerodynamics , Body-wing configurations , Computational fluid dynamics , Computerized simulation , Flow visualization , Grid generation (Mathematics) , Inlet flow , Three dimensional flow , Unstructured grids (Mathematics) , Air breathing engines , Engine inlets , Hypersonic flow , Inviscid flow , Transonic flow , Foreign technology
Demonstration of cluster computing for three-dimensional CFD simulations
Online Contents | 1999
|Fully automatic system for three-dimensional flow simulations
Online Contents | 1998
|