Development of a Vortex Particle Code for the Modeling of Wake Interaction in Distributed Propulsion
Author:
Affiliation:
1. Brigham Young University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3646
Reference56 articles.
1. Modeling Rotor Wakes with a Hybrid OVERFLOW-Vortex Method on a GPU Cluster
2. Modeling Rotor Wake Dynamics with Viscous Vortex Particle Method
3. A Finite State Dynamic Wake Model Enhanced with Vortex Particle Method–Derived Modeling Parameters for Coaxial Rotor Simulation and Analysis
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