Investigations of three over-the-rotor liner concepts at various technology readiness levels
Author:
Affiliation:
1. Acoustics Branch, NASA Glenn Research Center, Cleveland, OH, USA
2. Test Facility Management Facility Branch, NASA Glenn Research Center, Cleveland, OH, USA
3. Structural Acoustics Branch, NASA Langley Research Center, Hampton, VA, USA
Abstract
Publisher
SAGE Publications
Subject
Acoustics and Ultrasonics,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/1475472X211025803
Reference50 articles.
1. Huff DL. Noise reduction technologies for turbofan engines. In: Proceedings of inter-noise 2006, IN06 732, December 2006.
2. Hubbard HH (ed). Aeroacoustics of flight vehicles: theory and practice: volume 1: noise sources. NASA Reference Publication 1258, WRDC Technical Report 90-3052.
3. Jones MG, Parrott TL, Sutliff DL, et al. Assessment of soft vane and metal foam engine noise reduction concepts. AIAA-2009-3142.
4. Jones MG, Howerton BM. Evaluation of novel liner concepts for fan and airframe noise reduction. AIAA-2016-2787.
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