Computational Investigation of Conventional and Active-Flow-Control-Enabled High-Lift Configurations
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Dassault Systemes Simulia Corporation, Long Beach, California 90802
Funder
NASA Advance Air Vehicles Program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036233
Reference56 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. LoftinL. “Quest for Performance: The Evolution of Modern Aircraft,” NASA SP-468, 1985, https://www.hq.nasa.gov/pao/History/SP-468/ch10-5.htm.
3. The control of flow separation by periodic excitation
4. Actuators for Active Flow Control
5. Active Flow Control for Practical High-Lift Systems
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