Experimental Investigation of the HQ-Liner Concept on a Scale Simulated Turbofan Rig

Author:

Alonso Jose1,Burdisso Ricardo1,Kwan Hwa2,Byrne Stuart2,Chien Eugene2

Affiliation:

1. Virginia Polytechnic Institute and State University

2. Goodrich Corporation

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Design of sinusoidal-shaped inlet duct for acoustic mode modulation noise reduction of cooling fan;Applied Acoustics;2024-01

2. Side-branch resonators modelling with Green׳s function methods;Journal of Sound and Vibration;2014-09

3. Optimisation of axially segmented liners for aeroengine broadband noise;Journal of Sound and Vibration;2010-10

4. EVNERT Program: Testing of Adaptive HQ-Liner for Aft Noise Control;14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference);2008-05-05

5. Nonlinear Modeling of Shock Wave Trains in Ducts with Wall Discontinuities;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08

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