Noise Reduction Studies from the Leading Edge of Serrated Flat Plates-Reference-Cited by-同舟云学术

Noise Reduction Studies from the Leading Edge of Serrated Flat Plates

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Narayanan S.¹,Joseph Phillip¹,Haeri Sina¹,Kim Jae Wook¹

Affiliation:

1. University of Southampton

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2320

Reference14 articles.

1. Morphometric characterisation of wing feathers of the barn owl Tyto alba pratincola and the pigeon Columba livia

2. 2P.T. Soderman, "Aerodynamic effects of leading-edge serrations on a two- dimensional airfoil", Technical Report, NASA TM X-2643, 1972.

3. Application of a Beamforming Technique to the Measurement of Airfoil Leading Edge Noise

4. 4J. K. Staubs, "Real airfoil effects on leading edge noise", PhD dissertation, Virginia polytechnic institute and state university inAerospace Engineering.

5. Reduction of blade-vortex interaction noise through porous leading edge

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