Experimental investigation on the influence of liner non-uniformities on prevailing modes

Author:

Rademaker Edward1,Sarin Sohan2,Parente Charles3

Affiliation:

1. National Aerospace Lab., Emmeloord, Netherlands

2. Fokker Aircraft, Schiphol, Netherlands

3. Northrop Grumman Corp., Bethpage, NY

Publisher

American Institute of Aeronautics and Astronautics

Reference2 articles.

1. 'Sarin, S.L.,Rademaker, E.R.,In-flight Acoustic Mode Measurements in the Turbofan Engine Inlet of Fokker 100 Aircraft, AIAA-paper 93-4414

2. 2Zandbergen, T., Stator Vane Response due to the Impingement of the Wake of an Unloaded Rotor, AIAApaper 89-1125

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1. Eigenmodes of lined flow ducts with rigid splices;Journal of Fluid Mechanics;2011-11-28

2. The Virtual Scarf Inlet;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

3. Zero Splice Technology and Acoustic Benefits;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08

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