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1. 1. Addressing Adaptive Structure Technology to Reduce the Airframe Noise(Link)

   University essay from KTH/Hållfasthetslära (Avd.)

   Author : Hakan Sahin; [2012]
   Keywords : Adaptive Slat; Composite Slat; Airbus; DLR; Slat deformation; airframe noise;

   Abstract : ABSTRACTThe purpose of this thesis is to design and analyze the new generation leading edge slat of a commercial jet to reduce the structural noise with the application of new conceptual design approaches. Recent scientific research show that the leading edge slats account for the structural noise during the flight operation therefore, when the leading edge slat is deployed under different flight conditions, an open gap/slot is formed between the high lift device and the wing box. READ MORE