Application of through surface perforation for aircraft flow parameters control
Author:
Affiliation:
1. Bauman Moscow State Technical University,Special engineering,Moscow,Russian Federation
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10382256/10382242/10382276.pdf?arnumber=10382276
Reference11 articles.
1. Methods of reduction and calculation of nonstationary aerodynamic loads during keel buffeting of a maneuverable aircraft;Epikhin;Mathematical Modeling,2017
2. Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil;Purser;L-445, Landley,1941
3. Effects of design variables on spoiler control effectiveness, hinge moments, and wake turbulence
4. PIV investigation of flowfield behind perforated Gurney-type flaps
5. Aerodynamic Characteristics of Airfoil with Perforated Gurney-Type Flaps
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