System-Level Assessment of Active Flow Control for Commercial Aircraft High-Lift Devices
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034401
Reference23 articles.
1. Technology Assessment of NASA Environmentally Responsible Aviation Advanced Vehicle Concepts
2. Flow Separation Control on a Full-Scale Vertical Tail Model using Sweeping Jet Actuators
3. HartwichP. M.DickeyE. D.SclafaniA. J.CamachoP.GonzalesA. B.LawsonE. L.MairsR. Y.ShmilovichA. “AFC-Enabled Simplified High-Lift System Integration Study,” NASA CR-2014-218521, 2014.
4. System-Level Performance Impact of Active Flow Control Vertical Tails on a Commercial Transport Model Family
5. KuchanA. “The Integration of Active Flow Control Devices into Composite Wing Flaps,” M.S. Thesis, Georgia Inst. of Technology, Atlanta, GA, Aug. 2012, https://smartech.gatech.edu/handle/1853/44758 [retrieved 16 Oct. 2017].
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