Aerodynamic and Aeroacoustic Analysis of Installed Pusher-Propeller Aircraft Configurations
Author:
Affiliation:
1. DLR, German Aerospace Research Center, 38108 Braunschweig, Germany
2. Piaggio Aero Industries SpA, 80078 Pozzuoli, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031704
Reference18 articles.
1. CESAR (Cost Effective Small AiRcraft), Aug. 2012, http:// cordis.europa.eu/search/index.cfm?fuseaction=result.document&RS_ LANG;=FR&RS_RCN;=12280628&q;=.
2. Overview of the Hybrid RANS Code TAU
3. A one-equation turbulence model for aerodynamic flows
4. Comparison of eddy viscosity-transport turbulence models for three-dimensional, shock-separated flowfields
5. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
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