Multiple-Fidelity Modeling of Interactional Aerodynamics
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034709
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3. Some Conclusions from an Investigation of Blade‐Vortex Interaction
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5. Effects of Perpendicular Blade-Vortex Interaction, Part 2: Parameter Study
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