Paper
23 May 1997 Qualification of smart composites for use in aerospace applications
Ursula Herold-Schmidt, Erik Floeth, Baernd Last, Wolfgang Schaefer, Helmut W. Zaglauer
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Abstract
For smart materials to become widely used in aerospace applications, a number of stringent requirements concerning their performance in various operating environments have to be satisfied. Laboratory scale test procedures have been developed to assess the suitability of piezoceramic/carbon fiber reinforced plastic composites with embedded as well as surface-bonded actuators for active vibration and shape control of aerospace structures. In experimental and analytical investigations various composite configurations were evaluated with respect to the resulting actuation capability as well as the compatibility with various operation conditions.
© (1997) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ursula Herold-Schmidt, Erik Floeth, Baernd Last, Wolfgang Schaefer, and Helmut W. Zaglauer "Qualification of smart composites for use in aerospace applications", Proc. SPIE 3044, Smart Structures and Materials 1997: Industrial and Commercial Applications of Smart Structures Technologies, (23 May 1997); https://doi.org/10.1117/12.274660
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Cited by 12 scholarly publications.
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KEYWORDS
Actuators

Composites

Aerospace engineering

Ceramics

Semiconducting wafers

Ferroelectric materials

Active vibration control

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