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Volume 133
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10.3390/engproc2026133207
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Correction to Eng. Proc. 2026, 133(1), 150.
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Correction

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

by
Florian Mock
*,
Lukas Kettenhofen
,
Daniel Alboldt
and
Kai-Uwe Schröder
Institute of Structural Mechanics and Lightweight Design, RWTH Aachen University, Wüllnerstraße 7, 52066 Aachen, Germany
*
Author to whom correspondence should be addressed.
Eng. Proc. 2026, 133(1), 207; https://doi.org/10.3390/engproc2026133207
Published: 17 August 2026
(This article belongs to the Proceedings of The 15th EASN International Conference on “Innovation in Aviation & Space Towards Sustainability Today & Tomorrow”)
Browse Figures
Versions Notes
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In the original publication [1], unpublished details of the resonators were included.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.
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]
Engproc 133 00207 g001
Figure 1. Mounting brackets for energy harvesting resonators attached to a stiffened plate as a model for the airframe.
Figure 1. Mounting brackets for energy harvesting resonators attached to a stiffened plate as a model for the airframe.
Engproc 133 00207 g001
Engproc 133 00207 g002
Figure 2. (c) Modal hammer on the rear side, R: resonator position.
Figure 2. (c) Modal hammer on the rear side, R: resonator position.
Engproc 133 00207 g002
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MDPI and ACS Style

Mock, F.; Kettenhofen, L.; Alboldt, D.; Schröder, K.-U. Correction: Mock et al. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150. Eng. Proc. 2026, 133, 207. https://doi.org/10.3390/engproc2026133207

AMA Style

Mock F, Kettenhofen L, Alboldt D, Schröder K-U. Correction: Mock et al. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150. Engineering Proceedings. 2026; 133(1):207. https://doi.org/10.3390/engproc2026133207

Chicago/Turabian Style

Mock, Florian, Lukas Kettenhofen, Daniel Alboldt, and Kai-Uwe Schröder. 2026. "Correction: Mock et al. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150" Engineering Proceedings 133, no. 1: 207. https://doi.org/10.3390/engproc2026133207

APA Style

Mock, F., Kettenhofen, L., Alboldt, D., & Schröder, K.-U. (2026). Correction: Mock et al. Vibroacoustic Optimization of the Airframe Using Energy Harvesting Resonators: An Experimental and Numerical Approach. Eng. Proc. 2026, 133, 150. Engineering Proceedings, 133(1), 207. https://doi.org/10.3390/engproc2026133207

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