Features in Aerodynamic Characteristics and Flow Structures Around an Aircraft with Perforated Stabilizing Devices
Author:
Affiliation:
1. Bauman Moscow State Technical University,Faculty of Special Engineering,Moscow,Russia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10525678/10525705/10526126.pdf?arnumber=10526126
Reference32 articles.
1. Research of influence of perforation to reduce pulsation loads acting on the aerodynamic control surfaces;Kalugin;Civil Aviation High Technologies,2016
2. Control of separated and vortex flow using perforated aircraft surface
3. Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil;Purser;NACA report L-445. Langley Memorial Aeronautical Laboratory, Langley Field,1941
4. Aerodynamic Characteristics of Airfoil with Perforated Gurney-Type Flaps
5. CFD Analysis of NACA-0012 Airfoil with Various Porous Gurney Flap Geometries
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