In-flight acoustic mode measurements in the turbofan engine inlet of Fokker 100 aircraft
Author:
Affiliation:
1. Fokker Aircraft, Schiphol, Netherlands
2. National Aerospace Lab., Amsterdam, Netherlands
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-4414
Reference6 articles.
1. Zandbergen, T., Sarin, S.I. Laan, J.N. %cetiiiin\. H.J. "In-flight acoustic tiiotle and iiiipcdaiicc iiicii\ureinents in the engine intake of n Fokkcr F2R aircratt", AIAA-83-0677
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