Truncated Method for Propeller Noise Prediction up to Low Supersonic Helical Tip Mach Numbers
Author:
Affiliation:
1. Royal Military Academy
2. Ecole Centrale de Lyon
3. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3330
Reference38 articles.
1. Advanced turboprop noise prediction based on recent theoretical results
2. Multidisciplinary Design Optimization of a Quiet Propeller
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