Reynolds Number Effects on Transonic Designed Multi-Swept Combat Wing at Subsonic & Supersonic Speeds
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Jan 19, 2023
- Source ID
- 10.2514/6.2023-0821
Entities
People
- Mehdi Ghoreyshi
- Michel Van Rooij
- Raj Nangia
Organizations
- National Aerospace Laboratory
- United States Air Force Academy
- University of Bristol