The Effects of Segmented Piezoelectric Actuator Configuration on Aircraft Noise Control Performance
39th, Structures, structural dynamics, and materials conference ; 1998 ; Long Beach; CA
01.01.1998
8 pages
Aufsatz (Konferenz)
Englisch
materials , AHS , structures , adaptive structures , AIAA , ASME
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Piezoelectric Actuator Configuration Optimization for Active Structural Acoustic Control in Aircraft
SAE Technical Papers | 1997
|Optimization of Piezoelectric Actuator Grouping for Aircraft Cabin Noise Control
British Library Conference Proceedings | 2000
|Optimization of piezoelectric actuator grouping for aircraft cabin noise control
Tema Archiv | 2000
|