Testing of High-Lift Common Research Model with Integrated Active Flow Control
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Funder
Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035906
Reference46 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. The control of flow separation by periodic excitation
3. Actuators for Active Flow Control
4. McLeanJ. D.CrouchJ. D.StonerR. C.SakuraiS.SeidelG. E.FeifelW. M.RushH. M. “Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft,” NASA CR 1999–209338, 1999, https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990061938.pdf.
5. System-Level Trade Studies for Transonic Transports with Active Flow Control (AFC) Enhanced High-Lift Systems
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