ABSTRACT |
The CFD code, which is developed to analyze a flow around complex configurations with high resolution, is validated by two kinds of experimental data in order to establish reliability. One is a flow around an arrow wing, which is a simple configuration. Another is a flow around a wing-body configuration which simulate a next generation supersonic transport. Global properties as lift, drag and pitching moment are compared between experiment and computation, as well as pressure distributions on wing surfaces. These comparisons show good agreement |