Comparison of Computational Fluid Dynamics Hover Predictions on the S-76 Rotor
Author:
Affiliation:
1. U.S. Naval Air Systems Command, Patuxent River, Maryland 20670
2. High Performance Computing Modernization Program Computational Research and Engineering for Acquisition Tools and Environments-Air Vehicle, Lorton, Virginia 22079
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034121
Reference16 articles.
1. Capability Enhancements in Version 3 of the Helios High-Fidelity Rotorcraft Simulation Code
2. Application of Parallel Adjoint-Based Error Estimation and Anisotropic Grid Adaptation for Three-Dimensional Aerospace Configurations
3. Hover Predictions on the Sikorsky S-76 Rotor using Helios
4. Simulation of Rotor in Hover: Current State, Challenges and Standardized Evaluation
5. BalchD. T.LombardiJ. “Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interactions in Hover. Volume 1: Text and Figures,” NASA CR 177336, Feb. 1985.
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