Computational Investigation of Multirotor Interactional Aerodynamics with Hub Lateral and Longitudinal Canting
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, New York 12180
2. The Boeing Company, Ridley Park, Pennsylvania 19078
Funder
Boeing
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060530
Reference10 articles.
1. Computational Analysis of Multi-Rotor Flows
2. Ventura DiazP.YoonS. “High-Fidelity Computational Aerodynamics of Multi-Rotor Unmanned Aerial Vehicles,” AIAA SciTech Forum, AIAA Paper 2018-1266, 2018. 10.2514/6.2018-1266
3. Computational Study on Rotor Interactional Effects for a Quadcopter in Edgewise Flight
4. Industrial application of RANS modelling: capabilities and needs
5. Computational Study of Diffuser Length on Ducted Rotor Performance in Edgewise Flight
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