Theoretical developments in hypersonic turbulent boundary layers with application to friction and heat transfer estimation
Abstract
This project is focused on improving our theoretical description of high-speed turbulent boundary layers and to use this to develop more accurate engineering prediction tools. The work is centered around the development of near-wall scaling theory and the use of similarity analysis in the presence of non-zero pressure gradients. The project will also involve the creation of several direct numerical simulation data sets for validation at high Mach numbers.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Feb 29, 2024
- Source ID
- FA95502310228
Entities
People
- Johan Larsson
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Maryland