-Reference-Cited by-同舟云学术

Feasibility study to build a smart rotor: trailing edge flap actuation

Author:

Samak Dhananjay K.,Chopra Inderjit

Publisher

SPIE

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Introduction;Smart Helicopter Rotors;2015-12-16

2. Vibration Analysis of A Helicopter Blade with A Piezoelectric Actuated Trailing Edge Flap;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

3. Modeling and Flight Control of Large-Scale Morphing Aircraft;Journal of Aircraft;2007-07

4. Dynamic Behavior of Piezoelectric Recurve Actuation Architectures;Journal of Vibration and Acoustics;2004-01-01

5. Vibratory Loads Reduction Testing of the NASA/Army/MIT Active Twist Rotor;Journal of the American Helicopter Society;2002-04-01

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