Modeling and Prediction of Krueger Device Noise
Author:
Affiliation:
1. NEAT Consulting
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2957
Reference28 articles.
1. Guo Y. P., Nickol C. and Thomas R. H. "Noise and Fuel Burn Reduction Potential of an Innovative Subsonic TransportConfiguration," AIAAPaper 2014-0257.
2. Guo Y. P., Burley C.L. and Thomas R. H. "On Noise Assessment for Blended Wing Body (BWB) Aircraft," AIAAPaper 2014-0365.
3. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments
4. Pott-Pollenske M., Almoneit D. and Wild J. "On the Noise Generation of Krueger Leading Edge Devices," AIAA Paper2015-3142.
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