Quayle, AR and Quayle, AR and Dowling, AP and Dowling, AP and Dowling, AP and Babinsky, H and Babinsky, H and Babinsky, H and Graham, WR and Graham, WR and Graham, WR and Shin, HC and Shin, HC and Shin, HC and Sijtsma, P (2007) Landing gear for a 'silent' aircraft. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, 4. pp. 2709-2723.Full text not available from this repository.
The Silent Aircraft Initiative aims to provide a conceptual design for a large passenger aircraft whose noise would be imperceptible above the background level outside an urban airfield. Landing gear noise presents a significant challenge to such an aircraft. 1/10th scale models have been examined with the aim of establishing a lower noise limit for large aircraft landing gear. Additionally, the landing gear has been included in an integrated design concept for the 'Silent' Aircraft. This work demonstrates the capabilities of the closed-section Markham wind tunnel and the installed phased microphone arrays for aerodynamic and acoustic measurements. Interpretation of acoustic data has been enhanced by use of the CLEAN algorithm to quantify noise levels in a repeatable way and to eliminate side lobes which result from the microphone array geometry. Results suggest that highly simplified landing gears containing only the main struts offer a 12dBA reduction from modern gear noise. Noise treatment of simplified landing gear with fairings offers a further reduction which appears to be limited by noise from the lower parts of the wheels. The importance of fine details and surface discontinuities for low noise design are also underlined.
|Divisions:||Div A > Fluid Mechanics|
|Depositing User:||Cron job|
|Date Deposited:||16 Jul 2015 14:10|
|Last Modified:||29 Aug 2015 02:17|