Computations of Swept Wing Icing Aerodynamics
Author:
Affiliation:
1. University of Virginia, Charlottesville
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0328
Reference25 articles.
1. Ice-Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel
2. Ice-Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel
3. Effect of Ice Shape Fidelity on Swept Wing Aerodynamic Performance
4. Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulation Models for Flow Around an Iced Wing
5. Zonal Detached-Eddy Simulation of Turbulent Unsteady Flow over Iced Airfoils
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1. A subgrid model with multiple relaxation time for lattice Boltzmann method based on the Cartesian grid;Engineering Computations;2023-10-06
2. Three-Dimensional Flow Development on a 30° Swept Wing with Active Flow Control;AIAA AVIATION 2023 Forum;2023-06-08
3. Enhanced prediction of three-dimensional finite iced wing separated flow near stall;International Journal of Heat and Fluid Flow;2022-12
4. Non-Equilibrium Wall Modeling for Large Eddy Simulation of Stalled Iced Airfoils;AIAA Scitech 2020 Forum;2020-01-05
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