Suction and Pulsed Blowing Applied to Local Separation Downstream of Slat Cutout
Author:
Affiliation:
1. Tel Aviv University, 69978 Ramat Aviv, Israel
Funder
INAFLOWT
CS2
EU
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061004
Reference22 articles.
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3. Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
4. Active Separation Control at the Pylon-Wing Junction of a Real-Scale Model
5. Stall Behaviour of the EUROLIFT High Lift Configurations
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1. Experimental investigation of suction and oscillatory blowing as an alternative for a leading edge slat;Aerospace Science and Technology;2024-08
2. Active Flow Control as Means to Incorporate Virtual Slat Geometry;2023
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