Control of shock wave/boundary layer interactions in a supersonic air intake using a modified backward-facing step
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Aug 17, 2022
- Source ID
- 10.1007/s00193-022-01091-5
Entities
People
- Nikhil Khobragade
- Rajan Kumar
Organizations
- Air Force Research Laboratory