Turbine blade/vane interaction noise - Acoustic mode analysis using in-duct sensor rakes
Author:
Affiliation:
1. DLR, Inst. of Propulsion Technology, Berlin, Germany
2. MTU Aero Engines, Munich, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2153
Reference9 articles.
1. Experimental verification of a radial mode analysis technique using wall‐flush mounted sensors
2. NOISE SOURCE IDENTIFICATION IN A PROPFAN MODEL BY MEANS OF ACOUSTICAL NEAR FIELD MEASUREMENTS
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