Coupled uRANS and FW-H Analysis of Installed Pusher Propeller Aircraft Configurations
Author:
Affiliation:
1. DLR, German Aerospace Research Center
2. Piaggio Aero Industries SpA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3332
Reference17 articles.
1. Overview of the Hybrid RANS Code TAU
2. 3Spalart, P. and Allmaras, S. “A One-Equation Turbulence Model for Aerodynamic Flows,” Tech. Rep. AIAA 92-0439, 1992.
3. Comparison of eddy viscosity-transport turbulence models for three-dimensional, shock-separated flowfields
4. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
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