Comparative Study of Effects of Sweep and Humps on High-Speed Propeller Blades
Author:
Affiliation:
1. Department of Mechanical Engineering, Royal Military Academy, B-1000 Brussels, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052833
Reference30 articles.
1. Aeroacoustic and Aerodynamic Optimization of Aircraft Propeller Blades
2. MarinusB.RogerM.Van den BraembusscheR.BosschaertsW. “Multidisciplinary Optimization of Propeller Blades: Focus on the Aeroacoustic Results,” AIAA Paper 2011-2801, June 2011.
3. MarinusB. “Multidisciplinary Optimization of Aircraft Propeller Blades,” Ph.D. Thesis, Royal Military Academy, Brussels, Belgium, Nov. 2011.
4. Influence of Propeller Design Parameters on Far-Field Harmonic Noise in Forward Flight
5. Acoustic measurements of three Prop-Fan models
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