Computational Fluid Dynamics as a Support to Counter-Rotating Open-Rotor Wind-Tunnel Test Analysis
Author:
Affiliation:
1. Applied Aerodynamics Department, ONERA–The French Aerospace Lab, F-92190 Meudon, France
2. Computational Fluid Dynamics and Aeroacoustics Department, ONERA–The French Aerospace Lab, F-92322 Chatillon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032348
Reference9 articles.
1. “Advanced Turboprop Project,” NASA SP-495, April 1988.
2. Aero-mechanical optimization of a contra-rotating open rotor and assessment of its aerodynamic and acoustic characteristics
3. Acoustic tests of contra rotating propellers in the "Dream" project.
4. Computation of GOAHEAD configuration with Chimera assembly
5. Aeroacoustic integral methods, formulation and efficient numerical implementation
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