Design and Testing of Low Noise Landing Gears-Reference-Cited by-同舟云学术

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Design and Testing of Low Noise Landing Gears

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:11th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Dobrzynski Werner¹,Schöning Britta¹,Chow Leung-Choi²,Wood Chris³,Smith Malcolm⁴,Seror Christelle⁵

Affiliation:

1. Deutsches Zentrum für Luft- und Raumfahrt

2. Airbus UK

3. Baesystems Regional Aircraft

4. ISVR

5. Messier-Dowty SA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3008

Reference7 articles.

1. Validation of a Prediction Model for Aerodynamic Noise from Aircraft Landing Gears

2. Correction of open jet wind tunnel measurements for shear layer refraction

3. Atmospheric absorption of sound: Update

Cited by 20 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. An Aeroacoustic Study of the Nose Landing Gear with Emphasis on Steering Actuators, Torque Link and Tow Hook;AIAA Scitech 2020 Forum;2020-01-05

2. Review of landing gear acoustic research at Messier-Bugatti-Dowty;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27

3. Landing Gear Noise Prediction and Analysis for Tube-And-Wing and Hybrid-Wing-Body Aircraft;54th AIAA Aerospace Sciences Meeting;2016-01-02

4. Aircraft noise prediction;Progress in Aerospace Sciences;2014-07

5. Experimental and Numerical Study on Aerodynamic Noise Reduction of Cylindrical Rod with Bionic Wavy Surface;Applied Mechanics and Materials;2013-11

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