Active Flow Control of a Complex 3D Supersonic Multi-Stream Nozzle Flow
Abstract
In this effort, we propose to extend and demonstrate an active flow control strategy on a realistically complex three-dimensional (3D) high Reynolds number turbulent flow with the primary goal of reducing the adverse effects of large-scale and tonal flow unsteadiness.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Feb 22, 2024
- Source ID
- FA95502310019
Entities
People
- Mark Glauser
Organizations
- Air Force Office of Scientific Research
- Syracuse University
- United States Air Force