Microjet Configuration Sensitivities for Active Flow Control on Multi-Element High-Lift Systems
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. University of California Davis, Davis, California 95616
Funder
NASA’s Advanced Air Transport Technology
Boeing Commercial Airplanes
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035986
Reference49 articles.
1. Development of advanced circulation control wing high-lift airfoils
2. An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications
3. JenschC.PfingstenK. C.RadespielR.SchuermannM.HauptM.BaussS. “Design Aspects of a Gapless High-Lift System with Active Blowing,” Deutscher Luft- und Raumfahrtkongress, Vol. 58, 2009, pp. 168–189.
4. Active Control of Flow Seperation on a Swept Constant Chord Half Model in a High-Lift Configuration
5. High-Lift Performance Enhancement of a Simple Flap using Aerodynamic Flow Control
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1. Scoping of an Air Supply System for Active Flow Control on a Commercial Transport Airplane;AIAA SCITECH 2024 Forum;2024-01-04
2. Microjet Angle Sensitivity for Active Flow Control on Multi-Element High-Lift Systems;AIAA AVIATION 2023 Forum;2023-06-08
3. Wind Tunnel Experiment of Microjet-Based Flow Control on a Two-Dimensional Wing with Flap;Journal of Aircraft;2023-03
4. Aerodynamic Assessment of Surface-Normal Active Flow Control for Lift Enhancement on the High-Lift Common Research Model;AIAA SCITECH 2023 Forum;2023-01-19
5. Wind Tunnel Experiment of Microjet-based Flow Control on a Multi-Element High-Lift Airfoil;AIAA SCITECH 2022 Forum;2022-01-03
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