Simulation Methodologies of Engine Noise Shielding by Wings Within Conceptual Aircraft Design
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference21 articles.
1. Framework for Analyzing Aircraft Community Noise Impacts of Advanced Operational Flight Procedures
2. BertschL. “Noise Prediction Within Conceptual Aircraft Design,” Deutsches Zentrum für Luft-und Raumfahrt (DLR) TR DLR-FB-2013-20, Göttingen, 2013.
3. System Noise Assessment of a Tube-and-Wing Aircraft with Geared Turbofan Engines
4. Comparison of Aircraft Noise Models with Flyover Data
5. Validation of an integrated simulation model for aircraft noise and engine emissions
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