Large-eddy simulations of the flow on an aerofoil with leading-edge imperfections
Author:
Affiliation:
1. Queen's University, Kingston, Ontario, Canada
2. Barcelona Supercomputing Centre, Barcelona, Spain
Funder
Bombardier
Mitacs
Publisher
Informa UK Limited
Subject
General Physics and Astronomy,Mechanics of Materials,Condensed Matter Physics,Computational Mechanics
Link
https://www.tandfonline.com/doi/pdf/10.1080/14685248.2021.1973015
Reference105 articles.
1. Faust GK, Mangur P. Status report on a natural laminar-flow nacelle flight experiment – nacelle design. 1987. (NASA Technical Report N90-12550, NASA).
2. Obara CJ, Dodbele SS. Nacelle aerodynamic performance. 1987. (NASA Technical Report N90-12552, NASA).
3. Aircraft icing
4. AIRCRAFT ICING
5. Shaw RJ. Progress toward the development of an aircraft icing analysis capability. 1984. (NASA Technical Memorandum TM-83562, NASA).
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1. Numerical and experimental investigations of diffusion-induced boundary layer separation on aero-engine nacelles;International Journal of Heat and Fluid Flow;2024-10
2. Flow Separation in Airfoils with Rough Leading Edges;AIAA Journal;2023-05
3. Direct numerical simulation of transitional flow past an airfoil with partially covered wavy roughness elements;Physics of Fluids;2022-10
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