Wall Distance Effects on Transition to Turbulence in Low-Reynolds-Number Separated Flows
Author:
Affiliation:
1. Brown University, Providence, Rhode Island 02912
Funder
National Science Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060599
Reference34 articles.
1. Analysis of low Reynolds number separation bubbles using semiempirical methods
2. McMastersJ. H.HendersonM. L. “Low-Speed Single-Element Airfoil Synthesis,” TR, NASA Langley Research Center, 1979, https://ntrs.nasa.gov/citations/19790015719.
3. Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104–105)
4. Low Reynolds Number Aerodynamics of Leading-Edge Flaps
5. On the possibility (or lack thereof) of agreement between experiment and computation of flows over wings at moderate Reynolds number
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