Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced Boundary-Layer Transition in a Quiet Tunnel
Abstract
The proposed research is to design, build, test, and characterize the performance of a plasma-based flow-control system to delay crossflow-induced boundary-layer transition at hypersonic speeds under quiet flow.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Jul 15, 2016
- Source ID
- FA95501610320
Entities
People
- Thomas J. Juliano
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Notre Dame