Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading

Sung Soo Na, Liviu Librescu

Research output: Chapter in Book/Report/Conference proceedingChapter

Abstract

A study of optimal vibration control of aircraft wings carrying externally mounted stores and exposed to blast loading is presented. The wing structure is modelled as a thin-wailed beam of closed cross-section contour, and a number of non-classical features such as transverse shear, secondary warping, and anisotropy of the constituent materials are included. The wing structure can carry underwing and/or tip stores. The control is achieved via the use of actuating and sensing capabilities provided by piezoelectric devices which are bonded or embedded into the host structure. The cases of piezoactuators spread over the entire span of the structure, or in the form of a patch are considered, and issues related with the influence of patch location and size upon the vibration control efficiency of wings carrying external stores axe discussed. Other issues related with the minimization of the required input power and of those generated by the inclusion/discard in the quadratic performance index of time-dependent external excitations are also addressed.

Original languageEnglish
Title of host publicationProceedings of SPIE - The International Society for Optical Engineering
PublisherSociety of Photo-Optical Instrumentation Engineers
Pages498-509
Number of pages12
Volume3667
Publication statusPublished - 1999
Externally publishedYes
EventProceedings of the 1999 Smart Structures and Materials - Mathematics and Control in Smart Structures - Newport Beach, CA, USA
Duration: 1999 Mar 11999 Mar 4

Other

OtherProceedings of the 1999 Smart Structures and Materials - Mathematics and Control in Smart Structures
CityNewport Beach, CA, USA
Period99/3/199/3/4

Fingerprint

Vibration control
blasts
wings
aircraft
vibration
external stores
Piezoelectric devices
piezoelectric actuators
Anisotropy
inclusions
shear
anisotropy
optimization
cross sections
excitation

ASJC Scopus subject areas

  • Electrical and Electronic Engineering
  • Condensed Matter Physics

Cite this

Na, S. S., & Librescu, L. (1999). Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading. In Proceedings of SPIE - The International Society for Optical Engineering (Vol. 3667, pp. 498-509). Society of Photo-Optical Instrumentation Engineers.

Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading. / Na, Sung Soo; Librescu, Liviu.

Proceedings of SPIE - The International Society for Optical Engineering. Vol. 3667 Society of Photo-Optical Instrumentation Engineers, 1999. p. 498-509.

Research output: Chapter in Book/Report/Conference proceedingChapter

Na, SS & Librescu, L 1999, Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading. in Proceedings of SPIE - The International Society for Optical Engineering. vol. 3667, Society of Photo-Optical Instrumentation Engineers, pp. 498-509, Proceedings of the 1999 Smart Structures and Materials - Mathematics and Control in Smart Structures, Newport Beach, CA, USA, 99/3/1.
Na SS, Librescu L. Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading. In Proceedings of SPIE - The International Society for Optical Engineering. Vol. 3667. Society of Photo-Optical Instrumentation Engineers. 1999. p. 498-509
Na, Sung Soo ; Librescu, Liviu. / Optimal vibration control of adaptive aircraft wings carrying externally mounted stores and exposed to blast loading. Proceedings of SPIE - The International Society for Optical Engineering. Vol. 3667 Society of Photo-Optical Instrumentation Engineers, 1999. pp. 498-509
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