Characterizing Streamwise Development of Surface Roughness Effects on a Supersonic Boundary Layer
Author:
Funder
DoD SMART
NASA
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061623
Reference38 articles.
1. Surface Roughness Effects Nosetip Ablation Characteristics
2. Supersonic Boundary Layers with Periodic Surface Roughness
3. Response of supersonic turbulent boundary layers to local and global mechanical distortions
4. X-33 Hypersonic Boundary-Layer Transition
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