Investigation on landing gear shallow round cavity flow field and noise signature-Reference-Cited by-同舟云学术

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Investigation on landing gear shallow round cavity flow field and noise signature

Published:2016-05-27 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA/CEAS Aeroacoustics Conference
language:
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Author:

De La Puente Fernando¹,Sanders Laurent¹,Druault Philippe²,Vuillot Francois¹

Affiliation:

1. ONERA

2. Pierre and Marie Curie University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2774

Reference31 articles.

1. Rossiter, J. E., Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds, MinistryofAviation;RoyalAircraftEstablishment;RAE Farnborough,1964.

2. Depth effects on the flow features and noise signature of shallow cylindrical cavities at a Mach number of 0.25

Cited by 4 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. Flow features of shallow cylindrical cavities subject to grazing flow;Physics of Fluids;2022-02

2. Acoustic Prediction of LAGOON Landing Gear: Cavity Noise and Coherent Structures;AIAA Journal;2018-11

3. Investigation of the Ffowcs-Williams and Hawkings Analogy on an Isolated Landing Gear Wheel;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

4. New Unstructured Grid Strategies for Applications to Aeroacoustic Computations of the LAGOON, Landing Gear Model, Using the CEDRE Unstructured Flow Solver;23rd AIAA/CEAS Aeroacoustics Conference;2017-06-02

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