Vane Stagger Angle and Camber Effects in Fan Noise Generation
Author:
Affiliation:
1. National Aerospace Laboratory NLR, Amsterdam, the Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48549
Reference7 articles.
1. Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows
2. Effects of Inflow Distortion Profiles on Fan Tone Noise
3. Sound Generated by Rotor Wakes Interacting with a Leaned Vane Stator
4. A small Strouhal number analysis for acoustic wave-jet flow-pipe interaction
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