Structure and Modeling of Hypersonic Boundary Layers in Transitional and Turbulent Regimes
Abstract
This research program will use (spatially developing) direct numerical simulations toclarify these issues. The simulations will make use of a newly developed DNS code that hasbeen optimized for canonical geometries. We propose to concurrently conduct Reynoldsaveraged (RANS) and wall-modeled large eddy simulations (WMLES) of the DNS cong-urations in order to achieve a more rapid understanding of the turbulence modeling issues.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- May 02, 2017
- Source ID
- FA95501710157
Entities
People
- Pramod Subbareddy
Organizations
- Air Force Office of Scientific Research
- North Carolina State University
- United States Air Force