Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse

Liviu Librescu; Sungsoo Na; Piergiovanni Marzocca; Chanhoon Chung; Moon K. Kwak

doi:10.1016/j.jsv.2004.05.010

Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse

Liviu Librescu, Sungsoo Na, Piergiovanni Marzocca, Chanhoon Chung, Moon K. Kwak

Research output: Contribution to journal › Article › peer-review

43 Citations (Scopus)

Abstract

This paper concerns the active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and exposed to a blast pulse. The goal is to implement an active flap control capability to suppress the flutter instability and enhance the subcritical aeroelastic response to time-dependent external pulses. To this end, a combined control law is implemented and its performances toward suppressing flutter and reducing the vibrational level in the subcritical flight speed range is demonstrated.

Original language	English
Pages (from-to)	685-706
Number of pages	22
Journal	Journal of Sound and Vibration
Volume	283
Issue number	3-5
DOIs	https://doi.org/10.1016/j.jsv.2004.05.010
Publication status	Published - 2005 May 20

Bibliographical note

Funding Information:
L. Librescu and P. Marzocca would like to acknowledge the partial support by the NASA Langley Research Center through Grant NAG-1-02-011. S.S. Na and M.K. Kwak also acknowledge the partial support by the Basic Research Program of the Korea Science and Engineering Foundation, Grant No. R01-2002-000-00129-0. The authors express their indebtedness to the anonymous reviewers for the constructive comments and suggestions that have contributed to the improvement of the paper.

ASJC Scopus subject areas

Condensed Matter Physics
Mechanics of Materials
Acoustics and Ultrasonics
Mechanical Engineering

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10.1016/j.jsv.2004.05.010

Cite this

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abstract = "This paper concerns the active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and exposed to a blast pulse. The goal is to implement an active flap control capability to suppress the flutter instability and enhance the subcritical aeroelastic response to time-dependent external pulses. To this end, a combined control law is implemented and its performances toward suppressing flutter and reducing the vibrational level in the subcritical flight speed range is demonstrated.",

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Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse

Abstract

Bibliographical note

ASJC Scopus subject areas

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