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17 August 2026

Correction: Mock et al. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150

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Institute of Structural Mechanics and Lightweight Design, RWTH Aachen University, Wüllnerstraße 7, 52066 Aachen, Germany
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Author to whom correspondence should be addressed.
Error in Figure and Text Correction
In the original publication [1], unpublished details of the resonators were included. Consequently, two figures (Figure 1 and Figure 2c) and a paragraph describing the resonators have been revised. The corrected Figure 1 and Figure 2c appear below.
Figure 1. Mounting brackets for energy harvesting resonators attached to a stiffened plate as a model for the airframe.
Figure 2. (c) Modal hammer on the rear side, R: resonator position.
A correction has been made to 2. Materials and Methods, Paragraph 1:
“The resonator weighs 42.3 g including its mounting bracket, which is glued to the stiffened plate as shown in Figure 1.”
The authors state that the scientific conclusions are unaffected. This correction was approved by the Academic Editor. The original publication has also been updated.

Reference

  1. Mock, F.; Kettenhofen, L.; Alboldt, D.; Schröder, K.-U. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150. [Google Scholar] [CrossRef] [Scilit]
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