Wind-Tunnel Investigation on the Compressive-Sensing Technique for Aeroengine Fan Noise Detection-Reference-Cited by-同舟云学术

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Wind-Tunnel Investigation on the Compressive-Sensing Technique for Aeroengine Fan Noise Detection

Published:2018-09 Issue:9 Volume:56 Page:3536-3546
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bu Huanxian¹,Yu Wenjun²,Kwan Pok-Wang¹,Huang Xun³

Affiliation:

1. Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong, People’s Republic of China

2. Aero Engine Academy of China, 101304 Beijing, People’s Republic of China

3. State Key Laboratory of Turbulence, Peking University, 100871 Beijing, People’s Republic of China

Funder

Ministry of Industry and Information Technology of China

Collaboration Initiation Grant

National Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057261

Reference32 articles.

1. Propagation and Decay of Shock Waves in Turbofan Engine Inlets

2. Aircraft noise and its nearfield propagation computations

3. High-order schemes for predicting computational aeroacoustic propagation with adaptive mesh refinement

4. A controllable canonical form implementation of time domain impedance boundary conditions for broadband aeroacoustic computation

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