Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings

Sung Soo Na, Liviu Librescu

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

A structured tailoring and adaptive materials technology for controlling the dynamic response of aircraft wing structures is discussed. The wing structure was modeled as the doubly-tapered composite thin-walled beam including various non-classical features. The influence of patch location and size of piezoactuators upon the control efficiency of the structure span is investigated. The numerical results depicted the application of tailoring and optimal control upon the vibration response of nonuniform wing structures subjected to external pressure pulses.

Original languageEnglish
Title of host publicationCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
PublisherAIAA
Pages217-227
Number of pages11
Volume2
Publication statusPublished - 2000
Externally publishedYes
Event41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and ExhibitAIAA/ASME/AHS Adaptive Structures ForumAIAA Non-Deterministic Approaches ForumAIAA Space Inflatables Forum - Atlanta, GA, USA
Duration: 2000 Apr 32000 Apr 6

Other

Other41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and ExhibitAIAA/ASME/AHS Adaptive Structures ForumAIAA Non-Deterministic Approaches ForumAIAA Space Inflatables Forum
CityAtlanta, GA, USA
Period00/4/300/4/6

Fingerprint

Dynamic response
Composite materials

ASJC Scopus subject areas

  • Architecture

Cite this

Na, S. S., & Librescu, L. (2000). Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (Vol. 2, pp. 217-227). AIAA.

Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings. / Na, Sung Soo; Librescu, Liviu.

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 2 AIAA, 2000. p. 217-227.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Na, SS & Librescu, L 2000, Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings. in Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. vol. 2, AIAA, pp. 217-227, 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and ExhibitAIAA/ASME/AHS Adaptive Structures ForumAIAA Non-Deterministic Approaches ForumAIAA Space Inflatables Forum, Atlanta, GA, USA, 00/4/3.
Na SS, Librescu L. Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 2. AIAA. 2000. p. 217-227
Na, Sung Soo ; Librescu, Liviu. / Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 2 AIAA, 2000. pp. 217-227
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