Sensitivity of Rotorcraft Hover Predictions to Mesh Resolution in Strand Grid Framework
Author:
Affiliation:
1. Science and Technology Corporation, Moffett Field, California 94035
2. Parallel Geometric Algorithms, LLC, Sunnyvale, California 94087
3. U.S. Army Aviation Development Directorate, Moffett Field, California 9403
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056571
Reference27 articles.
1. A Dual-Mesh Unstructured Adaptive Cartesian Computational Fluid Dynamics Approach for Hover Prediction
2. Helicopter Aerodynamic Modeling of S-76 Rotor with Tip-Shape Variations: Review of AIAA Standardized Hover Evaluations
3. On Strand Grids for Complex Flows
4. Application of strand meshes to complex aerodynamic flow fields
5. Capability Enhancements in Version 3 of the Helios High-Fidelity Rotorcraft Simulation Code
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