Experimental and Computational Investigations of a Normal-Hole-Bled Supersonic Boundary Layer
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053956
Reference21 articles.
1. Inlet Flow Control Technology: Learning from History, Reinventing the Future
2. On supersonic-inlet boundary-layer bleed flow
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4. Modeling supersonic inlet boundary-layer bleed roughness
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4. Delayed Detached Eddy Simulation of Axisymmetric Turbulent Shock Wave Boundary Layer Interaction at Mach 2.5;AIAA SCITECH 2023 Forum;2023-01-19
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