Effects of Reynolds Number on Swept Shock-Wave/Boundary-Layer Interactions
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Oct 01, 2021
- Source ID
- 10.2514/1.j060293
Entities
People
- Andrew Baldwin
- Farrukh S. Alvi
- Lee Mears
- Rajan Kumar
Organizations
- Air Force Office of Scientific Research
- Florida State University