Computational Investigation of Nominally-Orthogonal Pneumatic Active Flow Control for High-Lift Systems
Author:
Affiliation:
1. University of California, Davis
2. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0559
Reference50 articles.
1. Comparison of Microjets with Microtabs for Active Aerodynamic Load Control
2. A simple atmospheric boundary layer model applied to large eddy simulations of wind turbine wakes
3. High-Lift Aerodynamics
4. The aerodynamic design of multi-element high-lift systems for transport airplanes
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