Effect of Surface Roughness Geometry on Boundary-Layer Transition and Far-Field Noise
Author:
Affiliation:
1. Delft University of Technology, 2629HS Delft, The Netherlands
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059335
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