Further Investigation on the Effect of Sweep on Parallel Vortical-Gust/Wing Interactions on a Finite Aspect-Ratio Wing
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference31 articles.
1. Implicit LES Computation of a Vortical-Gust/Wing Interaction for Transitional Flow
2. Impact of a Vortical Gust on the Aerodynamics of a Finite Aspect-Ratio Wing
3. Counterclockwise Vortical-Gust/Airfoil Interactions at a Transitional Reynolds Number
4. Effects of Vertical Position and Orientation on a Vortical-Gust/Airfoil Interaction at a Transitional Reynolds Number
5. Further Investigations of Vortical Gust/Airfoil Interactions at a Transitional Reynolds Number
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1. Exploration of High-Frequency Actuation on Gust Response Using Large Eddy Simulation;Journal of Fluids Engineering;2024-04-10
2. Gust Response Analysis Using the Kriging Method for Laminar Flow;AIAA Journal;2023-05
3. Sparse Identification of Nonlinear Gust Response in Laminar Flow;AIAA SCITECH 2023 Forum;2023-01-19
4. Response of a Laminar Transonic Airfoil to a Periodic Traverse Gust;AIAA SCITECH 2022 Forum;2022-01-03
5. Aeroelastic Gust Response Analysis Using Reduced Order Aerodynamics For Laminar Flow;AIAA SCITECH 2022 Forum;2022-01-03
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