Effect of Turbulence Modeling Selection Within Helios for Small Quadrotor Aerodynamics
Author:
Affiliation:
1. Boston University, Boston, Massachusetts 02215
2. U.S. Army Combat Capabilities Development Command, Aviation & Missile Center, Moffett Field, California 94035
Funder
Boston University Department of Mechanical Engineering
U.S. Army Technology Development Directorate - Aviation, DoD HPCMP Internship Program
National Science Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036410
Reference38 articles.
1. SankaranV.SitaramanJ.WissinkA.DattaA.JayaramanB.PotsdamM.MavriplisD.YangZ.O’BrienD.SaberiH.ChengR.HariharanN.StrawnR. “Application of the Helios Computational Platform to Rotorcraft Flowfields,” AIAA Paper 2010-1230, Jan. 2010. 10.2514/6.2010-1230
2. Overview of the Helios Version 2.0 Computational Platform for Rotorcraft Simulations
3. Overview of New Capabilities in Helios Version 9.0
4. Comparison of Computational Fluid Dynamics Hover Predictions on the S-76 Rotor
5. Sensitivity Study of High-Fidelity Hover Predictions on the Sikorsky S-76 Rotor
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