Experimental Investigation of Dynamic Flow Interactions in Shock-Induced Separated Corner Boundary Layers
Abstract
The overall goal of the proposed effort is to enhance the current knowledge of 3D shock/boundary layer interactions (SBLI) that initiate and sustain the unstart process. Considering the corner boundary layer interacting with an impinging shock contributes to unstart initiation, the objective of the first part of the proposed effort is to delineate the mechanisms that contribute to the dynamic growth of separated corner flows. The objective of the latter part of the proposed effort is to elucidate the dynamic interactions between a separated corner and primary flows; these interactions complete the unstart initiation and sustain the progress of unstart process.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501510296
Entities
People
- Venkateswaran Narayanaswamy
Organizations
- Air Force Office of Scientific Research
- North Carolina State University
- United States Air Force