Effect of Sweep on Dynamic Stall of a Pitching Finite-Aspect-Ratio Wing
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Aug 01, 2019
- Source ID
- 10.2514/1.j058206
Entities
People
- Daniel J. Garmann
- Miguel R. Visbal
Organizations
- Air Force Office of Scientific Research
- Air Force Research Laboratory