Characterizing the Flow Instability in Shockwave and Turbulent Boundary Layer Interactions
Abstract
To couple the team s direct numerical and large-eddy simulation capability and database with global stability to characterize the inviscid instability and its receptivity in STBLI, with and without real gas effects. DMD analysis will also be completed.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501510284
Entities
People
- Marie Martin
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Maryland