An overset-mesh approach for large-Eddy simulation of high-Reynolds number aerofoil flow
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Aug 09, 2018
- Source ID
- 10.1080/10618562.2018.1532505
Entities
People
- D. P. Rizzetta
- M. R. Visbal
Organizations
- Air Force Office of Scientific Research
- Air Force Research Laboratory
- United States Department of Defense