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Complex Landing Gear Noise Prediction Using a Simple Toolkit

  • Published:2005-01-10 Issue: Volume: Page:
  • ISSN:
  • Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Lopes Leonard1,Brentner Kenneth1,Morris Phillip1,Lilley Geoffery1,Lockhard David2

Affiliation:

1. Pennsylvania State University

2. NASA Langley

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. 1Macaraeg, M. G. “Fundamental investigations of airframe noise,” AIAA Paper No. 98-2224.

2. 3Fink, M. R. “Component method for airframe noise,” FAA-RD-77-29. Available from DTIC as AD A039 664.

3. Noise Component Method for Airframe Noise

4. Sound Radiation from Aircraft Wheel-WelVLanding-Gear Configurations

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1. An Efficient Far‐Field Noise Prediction Framework for the Next Generation of Aircraft Landing Gear Designs;Advanced Multifunctional Lightweight Aerostructures; Design, Development, and Implementation;2021-02-12

2. Development of an empirical model for landing gear noise prediction;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 aeroacoustics of a two-strut, two-wheel landing gear in a propeller wake;52nd Aerospace Sciences Meeting;2014-01-10
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