A Comprehensive Study of Shock-wave-boundary-layer Interactions on Curved Surfaces
Abstract
To guide the design and control of future flight vehicles, it is therefore very important tounderstand the aero/thermodynamic effects of the SBLIs on curved surfaces. Although much has been learned, the complex dynamics of such systems has made the development of shock detection scheme challenging. The problem is challenging and requires a multi-pronged, interdisciplinary approach.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Jul 28, 2017
- Source ID
- FA95501710269
Entities
People
- Kumar Rajan
Organizations
- Air Force Office of Scientific Research
- Florida A&M University
- United States Air Force