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Hypersonic vehicles must be designed to tolerate the high temperatures experienced at hypersonic speeds. Ablation is one type of thermal protection system used on hypersonic vehicles. We present experimental results that show how ablation affects aerodynamics under certain conditions.

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This page is a summary of: Boundary-Layer Instabilities on Variable Bluntness Cones with Outgassing in Hypersonic Quiet Flow, AIAA Journal, June 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j065085.
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