Generation and Propagation of Multiple Pure Tones Inside Turbofans at Transonic Regime
Author:
Affiliation:
1. Computational Fluid Dynamics and Aeroacoustics Department, ONERA—The French Aerospace Lab, F-92322 Châtillon, France
2. Acoustics Department, Safran–Snecma, F-77550 Villaroche, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054007
Reference21 articles.
1. A Determination of the Wave Forms and Laws of Propagation and Dissipation of Ballistic Shock Waves
2. SofrinT.PickettG. “Multiple Pure Tone Noise Generated by Fans at Supersonic Tip Speeds,” NASA Tech. Rept. SP-304, 1970, pp. 435–459.
3. The Buzz-Saw Noise Generated by a High Duty Transonic Compressor
4. Shock Wave Behavior in Transonic Compressor Noise Generation
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