Turbulent Heat Flux Model for Hypersonic Shock–Boundary Layer Interaction
Author:
Affiliation:
1. Indian Institute of Technology Bombay, Mumbai 400 076, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference21 articles.
1. Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability
2. Uncertainty Assessments of Hypersonic Shock Wave-Turbulent Boundary-Layer Interactions at Compression Corners
3. Role of Turbulent Prandtl Numbers on Heat Flux at Hypersonic Mach Numbers
4. Evaluation of Turbulence Modeling Extensions for the Analysis of Hypersonic Shock Wave Boundary Layer Interactions
5. Modelling of turbulent energy flux in canonical shock-turbulence interaction
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