Dynamic response of adaptive cantilevers carrying external stores and subjected to blast loading

This paper deals with the control of the dynamic response of cantilevered thin-walled beams carrying externally mounted stores and exposed to time-dependent external excitations. In this context, and toward this goal, the adaptive materials technology is used. A feedback control law relating the piezoelectrically induced bending moment at the beam tip with the angular velocity at the same point of the structure is considered, and its effects on the closed-loop dynamic response is investigated. The obtained results reveal that this control methodology can play a noticeable role toward confining the oscillations of the considered structure when exposed to blast loadings.

[1]  L. Librescu,et al.  Integrated structural tailoring and control using adaptive materials for advanced aircraft wings , 1996 .

[2]  Leonard Meirovitch,et al.  Control of Cantilever Vibration via Structural Tailoring and Adaptive Materials , 1997 .

[3]  Ohseop Song,et al.  Adaptive vibrational behavior of cantilevered structures modeled as composite thin-walled beams , 1993 .

[4]  Malcolm J. Crocker Multimode Response of Panels to Normal and to Traveling Sonic Booms , 1967 .

[5]  Elmar Breitbach,et al.  Structronic systems : smart structures, devices and systems , 1998 .

[6]  Ohseop Song,et al.  Adaptive Response Control of Cantilevered Thin-Walled Beams Carrying Heavy Concentrated Masses , 1994 .

[7]  Victor Birman,et al.  Behaviour of laminated plates subjected to conventional blast , 1987 .

[8]  Don Berlincourt,et al.  3 – Piezoelectric and Piezomagnetic Materials and Their Function in Transducers , 1964 .

[9]  I. Lottati,et al.  Aeroelastic stability characteristics of a composite swept wing withtip weights for an unrestrained vehicle , 1987 .

[10]  Ohseop Song,et al.  Bending vibrations of adaptive cantilevers with external stores , 1996 .

[11]  L. Meirovitch Principles and techniques of vibrations , 1996 .

[12]  Allan D. Pierce,et al.  Physical acoustics : principles and methods , 1965 .

[13]  H. Tzou Piezoelectric Shells: Distributed Sensing and Control of Continua , 1993 .

[14]  A. Gjelsvik,et al.  The Theory of Thin-Walled Bars , 1981 .

[15]  L. Librescu,et al.  Response of laminated composite flat panels to sonic boom and explosive blast loadings , 1990 .

[16]  David V. Ritzel,et al.  Analytical study of sonic boom from supersonic projectiles , 1988 .

[17]  Edward F. Crawley,et al.  Aeroelastic actuation using elastic and induced strain anisotropy , 1995 .

[18]  Liviu Librescu,et al.  Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores , 1998 .

[19]  T. Bailey,et al.  Distributed Piezoelectric-Polymer Active Vibration Control of a Cantilever Beam , 1985 .

[20]  Liviu Librescu,et al.  Effects of externally mounted stores on aeroelasticity of advanced swept cantilevered aircraft wings , 1998 .

[21]  Amr M. Baz,et al.  Boundary Control of Beams Using Active Constrained Layer Damping , 1997 .

[22]  Edward F. Crawley,et al.  Intelligent structures for aerospace - A technology overview and assessment , 1994 .

[23]  Liviu Librescu,et al.  Vibration and dynamic response control of cantilevers carrying externally mounted stores , 1997 .