Theoretical Prediction of Roll Moment Due to Sideslip for Thin Low-Aspect-Ratio Wings
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Apr 01, 2019
- Source ID
- 10.2514/1.j057160
Entities
People
- Kamran Mohseni
- Thomas Linehan
Organizations
- Air Force Office of Scientific Research
- National Science Foundation
- University of Florida