Influence of Nonflat Plate Trailing Edge Serration on Airfoil Noise Reduction-Reference-Cited by-同舟云学术

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Influence of Nonflat Plate Trailing Edge Serration on Airfoil Noise Reduction

Published:2024-03 Issue:2 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sumesh C. K.¹,Jothi T. J. Sarvoththama²^ORCID

Affiliation:

1. Ph.D. Student, Dept. of Mechanical Engineering, National Institute of Technology Calicut, Kozhikode, Kerala 673601, India.

2. Associate Professor, Dept. of Mechanical Engineering, National Institute of Technology Calicut, Kozhikode, Kerala 673601, India (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4995

Reference43 articles.

1. Flow topology and acoustic emissions of trailing edge serrations at incidence;Arce León C.;Exp. Fluids,2016

2. Effects of trailing edge bluntness on airfoil tonal noise at low Reynolds numbers

3. Three-dimensional flow field over a trailing-edge serration and implications on broadband noise

4. Blake, W. K. 1986. Mechanics of flow induced sound and vibration. Orlando, FL: Academic Press.

5. Scaling of airfoil self-noise using measured flow parameters

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