In this paper the capabilities of an automated Computational Fluid Dynamics (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
1997
24 pages
Report
No indication
English
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