The Effects Of Strong Wall Cooling On Supersonic And Hypersonic Shock/Boundary-Layer Interactions
Abstract
The aim of the proposed work is to develop a physical understanding of the effects of wall cooling in supersonic and hypersonic shock/boundary-layer interactions. Shock/boundary-layer interactions (SBLI) are important in many high-speed flight applications. A sufficiently strong shock can separate the boundary layer, leading to loss of lift or control authority (in external flows) or to the initiation of unstart (in internal flows). Even during stable operation, SBLI may generate low-frequency oscillations that adversely affect the structure through unsteady structural- and heat-loads.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Dec 05, 2016
- Source ID
- FA95501610385
Entities
People
- Johan Larsson
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Maryland