Dynamic Deployment of a Minitab for Aerodynamic Load Control
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0405
2. University of Bath, Bath, England BA2 7AY, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. HeathcoteD. J. “Aerodynamic Loads Alleviation Using Mini-Tabs,” Ph.D. Thesis, Univ. of Bath, Bath, England, U.K. 2017.
2. An Experimental Study of Mini-Tabs for Aerodynamic Load Control
3. Aerodynamic Load Alleviation Using Minitabs
4. Active Gurney Flaps: Their Application in a Rotor Blade Centrifugal Field
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