Numerical Study of Transitional SD7003 Airfoil Interacting with Canonical Upstream Flow Disturbances
Author:
Affiliation:
1. Embry-Riddle Aeronautical University, Daytona Beach, Florida 32114
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055900
Reference41 articles.
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2. Editorial
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4. OlM. “The High-Frequency, High-Amplitude Pitch Problem: Airfoils, Plates and Wings,” AIAA Paper 2009-3686, 2009.
5. BaikY. S.RauschJ.BernalL.OlM. “Experimental Investigation of Pitching and Plunging Airfoils at Reynolds Number Between 1×104 and 6×104,” AIAA Paper 2009-4030, 2009.
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