High-Fidelity Computational Aerodynamics of Multi-Rotor Unmanned Aerial Vehicles
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1266
Reference19 articles.
1. Solver and Turbulence Model Upgrades to OVERFLOW 2 for Unsteady and High-Speed Applications
2. High Order Accurate Finite-Difference Methods: as seen in OVERFLOW
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