The low values of the x-crossflow term on the forebody suggest that most of the velocity is axial in the forebody a#39;vortexa#39;, ... The results indicate the medium grid, Run 5, produced essentially the same prediction of the peak suction in the forebody vortex and its location spanwise as the fine grid, Run 6. ... This is unusual in that in general Euler codes tend to over-predict the level of suction for these flows.
|Title||:||Euler Technology Assessment program for preliminary aircraft design employing SPLITFLOW code with Cartesian unstructured grid method|
|Author||:||Dennis B. Finley|