Open-Loop Hover Testing of a Smart Rotor Model-Reference-Cited by-同舟云学术

Open-Loop Hover Testing of a Smart Rotor Model

Published:2002-08 Issue:8 Volume:40 Page:1495-1502
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Koratkar Nikhil A.¹,Chopra Inderjit¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1834

Reference21 articles.

1. 1Jacklin, A., Nguyen, K., Blaas, A., and Richter, P. “Full-Scale Wind Tunnel Test of a Helicopter Individual Blade Control System,” 50thAmerican Helicopter Society Forum, American HelicopterSociety, Alexandria, VA,1994, pp.579-596.

2. Design of a servo-flap rotor for reduced control loads

3. Analysis and Testing of a Froude Scaled Helicopter Rotor with Piezoelectric Bender Actuated Trailing Edge Flaps

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