HIGHLIGHTS
- who: Dominique Charbonnier from the Switzerland Switzerland Switzerland Switzerland have published the Article: Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration, in the Journal: (JOURNAL)
- what: For the purpose of the present study, it is concluded that the default mesh with 2 million cells for each grid fin provides an acceptable accuracy with respect to the huge increase of computational resources that would be required Force ΔForce vs. default by the finer meshes. The aim of these simulations was to assess the efficiency of different aerodynamic control surfaces, and, in . . .
If you want to have access to all the content you need to log in!
Thanks :)
If you don't have an account, you can create one here.