Local-Variable-Based Transition Model for Hypersonic Flows Considering Wall Mass Injection
AIAA JOURNAL（2024）
Key words
Ablative Materials,Heat Transfer,Pyrolysis,Numerical Simulation,Freestream Mach Number,Reynolds Averaged Navier Stokes,Thermal Control and Protection,Boundary Layer Transition,Hypersonic Flows,Hypersonic Ablation
AI Read Science
Must-Reading Tree
Example
Generate MRT to find the research sequence of this paper
Chat Paper
Summary is being generated by the instructions you defined