Rotor wake and flow analysis using a coupled Eulerian–Lagrangian method
Author:
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Subject
Modelling and Simulation,General Computer Science
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2016.1174887
Reference28 articles.
1. Helicopter rotor blade computation in unsteady flows using moving overset grids
2. Rotor Free‐Wake Modeling Using a Pseudo‐Implicit Technique — Including Comparisons with Experimental Data
3. Development of a CFD-Based Hover Performance Prediction Tool for Engineering Analysis
4. Application of Computational Fluid Dynamics/Computational Structural Dynamics Coupling for Analysis of Rotorcraft Airloads and Blade Loads in Maneuvering Flight
5. Efficient High-Resolution Wake Modeling Using the Vorticity Transport Equation
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