Parametric Airfoil Design and Sensitivity Analysis for Turbulent Boundary-Layer Trailing-Edge Noise Reduction

Title
Parametric Airfoil Design and Sensitivity Analysis for Turbulent Boundary-Layer Trailing-Edge Noise Reduction
Authors
Keywords
-
Journal
AIAA JOURNAL
Volume -, Issue -, Pages 1-18
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2021-10-14
DOI
10.2514/1.j060096

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