Development and Analysis-Driven Optimization of Superelastic Slat-Cove Fillers for Airframe Noise Reduction
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3141
2. NASA Langley Research Center, Hampton, Virginia 23681-2199
3. Analytical Mechanics Associates, Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054011
Reference26 articles.
1. Effects of Geometric Details on Slat Noise Generation and Propagation
2. Aerodynamic Noise Reduction for High-Lift Devices on a Swept Wing Model
3. HorneW.JamesK.ArledgeT.SodermanP.BurnsideN.JaegerS. “Measurements of 26 Percent-Scale 777 Airframe Noise in the NASA Ames 40 by 80 Foot Wind Tunnel,” AIAA Paper 2005-2810, 2005.
4. Designing of Slat Cove Filler as a Noise Reduction Device for Leading-edge Slat
5. Lightweight Shape-Adaptable Airfoils: A New Challenge for an Old Dream
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