Multi-Disciplinary Computational Aerodynamics
Abstract
High-fidelity simulation was employed to address several complex unsteady interactions important to future USAF air vehicles. The research described in this report was focused on three key elements: 1. Vortex interactions in formation flight. 2. Dynamic stall. 3. Plasma-based transition control.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 2016
- Accession Number
- AD1001359
Entities
People
- Miguel R. Visbal
Organizations
- Air Force Research Laboratory