Dynamic Deployment of a Minitab for Aerodynamic Load Control

Author:

Heathcote D. J.1,Gursul I.2,Cleaver D. J.2

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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