WebOct 3, 2012 · On noise reduction by flap side edge fences. Journal of Sound and Vibration, Vol. 277, No. 1-2. Development of Computational Aeroacoustics Tools for Airframe Noise Calculations. International Journal of Computational Fluid Dynamics, Vol. 18, No. 6. Reduction of Flap Side-Edge Noise: Passive and Active Flow Control. WebJan 1, 2015 · Flap Edge Noise Reduction Fins [Khorrami, Mehdi R.] on Amazon.com. *FREE* shipping on qualifying offers. Flap Edge Noise Reduction Fins
Aeroacoustic Evaluation of Flap and Landing Gear Noise …
WebMay 1, 2024 · According to the noise reduction law for serrations proposed by Gruber et al. [15], a serration size with 2 h / c = 0.15 and λ / ( 2 h) = 0.5 is selected to satisfy the noise reduction criterion. Due to the deflection angle at the trailing edge of the wind turbine airfoil, the flap angle of the serration is not installed horizontally. green factory srl
Experimental investigation of porous materials for trailing-edge noise ...
WebNASA's Langley Research Center has developed aircraft flap tip modifications that reduce noise produced during approach and landing. The modifications are rigid open lattice (honeycomb-like) and fin structures (closely packed columns) that delay the formation of a noise-generating vortex at the flap side edge. WebSep 1, 2024 · The aircraft concept selected to achieve this goal is a high-lift system equipped with an active flow-control non-slotted flap and a droop nose. For this specific configuration, trailing edge noise becomes a dominant noise source. Porous materials as a passive means for trailing-edge noise reduction are selected and characterized. WebSimilarly, deflectors for the landing gear bay can also be applied along with landing gear mesh fairings. Porous devices along with flap edge noise reduction fins can be applied at the edge of flaps and tip of an aircraft flap so as to reduce flap side edge noise and airframe noise. Measures such as width reduction of slat gap can be implemented … green factory singapore