Acoustic Liner Drag: Measurements on Novel Facesheet Perforate Geometries
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2979
Reference8 articles.
1. 2Drouin, M. K.,Gallman, J. M., and Olsen, R.F. "Sound Level Effect on Perforated Panel Boundary Layer Growth," AIAA Paper2006-2411, May2006.
2. 3Thomas, R. H., Burley, C. L., Lopes, L. V., Bahr, C. J., Gern, F. H. and Van Zante, D. E. "System Noise Assessment and thePotential for aLowNoiseHybrid WingBodyAircraft with Open RotorPropulsion,"AIAAPaper 2014-0258, January2014.
3. 4Nikuradse,J."LawsofFlowinRoughPipes,"NACATM-1292,November1950.
4. 5Howerton, Brian M., and Jones, Michael G. "Acoustic Liner Drag: A Parametric Study of Conventional Configurations," AIAAPaper 2015-2230,21stAIAA/CEASAeroacousticsConference,AIAAAviation2015,June2015.
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