Numerical study of the influence of non-uniform wall temperature distribution on the hypersonic flow over a flat plate
Author:
Affiliation:
1. University of New South Wales
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2427
Reference26 articles.
1. Hot-Wall Reentry Testing in Hypersonic Impulse Facilities
2. Temperature and Heat Flux Measurement on Hot Models in Short-Duration Facilities
3. Comparison of Carbon Ablative Shock-Layer Radiation with High Surface Temperatures
4. Expansion Tunnel Experiments of Earth Reentry Flow with Surface Ablation
5. Analysis and Rebuilding of Experiments on a heated carbon graphite model in the X2 expansion tube
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