Unstructured Overset Mesh Adaptation with Turbulence Modeling for Unsteady Aerodynamic Interactions
Author:
Affiliation:
1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
2. Computational Aerosciences Branch, NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032195
Reference41 articles.
1. Comparison of Rotor-Airframe Interaction Utilizing Overset and Unstructured Grid Techniques
2. O’BrienD. M. “Analysis of Computational Modeling Techniques for Complete Rotorcraft Configurations,” Ph.D. Thesis, Georgia Inst. of Technology, Atlanta, 2006.
3. A Review of Rotor Wake Physics and Modeling
4. Effect of Wake Adaptation on Rotor Hover Simulations Using Unstructured Meshes
5. Unstructured Mesh Navier-Stokes Calculations of the Flow Field of a Helicopter Rotor in Hover
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