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Base de données et galerie internationale d'ouvrages d'art et du génie civil

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Smart Materials and Structures - v. 10, n. 1 (février 2001)

Publié:	février 2001

Articles dans ce numéro

Auteur(s)	Titre	Page(s)
Bernhard, Andreas P. F. / Chopra, Inderjit	Analysis of a bending-torsion coupled actuator for a smart rotor with active blade tips	35-52
Pelinescu, I. / Balachandran, B.	Analytical study of active control of wave transmission through cylindrical struts	121-136
Chen, Peter C. / Baeder, James D. / Evans, Robert A. D. / Niemczuk, John	Blade-vortex interaction noise reduction with active twist smart rotor technology	77-85
Samuel, Paul D. / Pines, Darryll J.	Classifying helicopter gearbox faults using a normalized energy metric	145-153
Lee, Taeoh / Chopra, Inderjit	Design of piezostack-driven trailing-edge flap actuator for helicopter rotors	15-24
Straub, F. K. / Ngo, H. T. / Anand, V. / Domzalski, D. B.	Development of a piezoelectric actuator for trailing edge flap control of full scale rotor blades	25-34
Cesnik, Carlos E. S. / Shin, SangJoon / Wilbur, Matthew L.	Dynamic response of active twist rotor blades	62-76
Revivo, Michael / Rand, Omri	Feasibility of non-rotating active lifting surface for helicopter vibration reduction	154-171
Epps, Jeanette J. / Chopra, Inderjit	In-flight tracking of helicopter rotor blades using shape memory alloy actuators	104-111
Gandhi, Farhan / Wang, K. W. / Xia, Liba	Magnetorheological fluid damper feedback linearization control for helicopter rotor application	96-103
Kube, R. / Klöppel, V.	On the role of prediction tools for adaptive rotor system developments	137-144
Cesnik, Carlos E. S. / Shin, SangJoon	On the twist performance of a multiple-cell active helicopter blade	53-61
Anusonti-Inthra, Phuriwat / Gandhi, Farhan	Optimal control of helicopter vibration through cyclic variations in blade root stiffness	86-95
Baz, A. / Ro, J.	Vibration control of rotating beams with active constrained layer damping	112-120
Koratkar, Nikhil A. / Chopra, Inderjit	Wind tunnel testing of a Mach-scaled rotor model with trailing-edge flaps	1-14

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IssueID
21225
Publié(e) le:
04.12.2018
Modifié(e) le:
03.08.2019

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