Influence of a Forward-Facing Step Surface Irregularity on Swept Wing Transition
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference28 articles.
1. AIRCRAFT LAMINAR FLOW CONTROL
2. Aircraft drag reduction—a review
3. Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements
4. Effect of surface steps on boundary layer transition
5. Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer
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