Numerical Investigation of Flow Control Using Vertex Generator for Landing Gear Noise Reduction (AIAA 2016-2773)
Aeroacoustics (Conference)
2016-01-01
10 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
The Reduction of Main Landing Gear Noise (AIAA 2016-2900)
British Library Conference Proceedings | 2016
|DataCite | 1898
Potential for Landing Gear Noise Reduction on Advanced Aircraft Configurations (AIAA 2016-3039)
British Library Conference Proceedings | 2016
|Mesh Screen Application for Noise Reduction of Landing Gear Strut (AIAA 2016-2845)
British Library Conference Proceedings | 2016
|