Some Insights into the Screech Tone of Under-Expanded Supersonic Jets Using Dynamic Mode Decomposition-Reference-Cited by-同舟云学术

Some Insights into the Screech Tone of Under-Expanded Supersonic Jets Using Dynamic Mode Decomposition

Published:2021-07 Issue:4 Volume:34 Page:04021034
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zang B.¹^ORCID,Vevek U. S.²,New T. H.³

Affiliation:

1. Lecturer, Faculty of Engineering, Univ. of Bristol, Bristol BS8 1TR, UK. ORCID: .

2. Research Associate, School of Mechanical and Aerospace Engineering, Nanyang Technological Univ., Singapore 639798, Singapore.

3. Associate Professor, School of Mechanical and Aerospace Engineering, Nanyang Technological Univ., Singapore 639798, Singapore (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001286

Reference51 articles.

1. Broadband Shock-Associated Noise in Screeching and Non-Screeching Underexpanded Supersonic Jets

2. Assunção T. L. V. Jaunet Y. Gervais and G. Stève. 2019. “Closure mechanism investigation of axisymmetric and helical screech modes in underexpanded round jets.” In Proc. INTER-NOISE and NOISE-CON Congress and Conf. Proc. Madrid Spain: Institute of Noise Control Engineering.

3. The Proper Orthogonal Decomposition in the Analysis of Turbulent Flows

4. Current Status of Jet Noise Predictions Using Large-Eddy Simulation

5. Unstructured Large-Eddy Simulations of Supersonic Jets

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