Demonstration of AM Rapid Prototyping for Hypersonic Boundary Layer Experimentation
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of Dayton Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0941
Reference15 articles.
1. 3D-Printed Quasi-Random Distributed Roughness for Turbulent Boundary Layer Analysis on Hypersonic Ogive Nosecones
2. Fin-induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5
3. Experimental measurements and numerical investigations of boundary-layer instabilities on a Mach 5 hollow cylinder
4. Hypersonic Ground Tests In Support of the Boundary Layer Transition (BOLT) Flight Experiment
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