Numerical study of blunt leading edge separation on a 53 degree swept diamond wing (STO AVT-183) using the Edge and Cobalt flow solvers
53rd AIAA Aerospace Sciences Meeting
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
|Swept wing effects on Wavy Leading Edge Phenomena
AIAA | 2018
|