2018
DOI: 10.1088/1757-899x/290/1/012054
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Energy Harvesting from Aerodynamic Instabilities: Current prospect and Future Trends

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Cited by 11 publications
(11 citation statements)
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“…A review of the current prospects and future trends for aerodynamic EH in aircraft applications, with considerations on the layout and advancement of EH devices based on aerodynamic instabilities, was recently performed [ 41 ]. The underlying principles rely generally on airflow (von Karman) vortices induced by obstacles (i.e., bluff bodies) or aerofoil sections that induce the fluttering or galloping of structures placed in such an environment (cf.…”
Section: Airflow and Acoustic Energy Harvesting Systemsmentioning
confidence: 99%
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“…A review of the current prospects and future trends for aerodynamic EH in aircraft applications, with considerations on the layout and advancement of EH devices based on aerodynamic instabilities, was recently performed [ 41 ]. The underlying principles rely generally on airflow (von Karman) vortices induced by obstacles (i.e., bluff bodies) or aerofoil sections that induce the fluttering or galloping of structures placed in such an environment (cf.…”
Section: Airflow and Acoustic Energy Harvesting Systemsmentioning
confidence: 99%
“…In case of the herein considered fixed wing aircraft, due to their abundance on the airplane and some of its typical structural elements ( Figure 3 ), mechanical vibrations (including that induced by the flow of air around the airplane) and thermal gradients, used separately or, to increase the possibility of providing the required energy constantly and reliably, simultaneously, are considered as the most promising sources for EH-based autonomous SHM sensor nodes [ 8 , 41 , 42 , 43 ]. Although some initial studies of integrated SHM solutions, combining advanced microelectronics with sensors, EH devices, power management, time synchronization, and web-based data distribution, have been proposed [ 44 ], due to the often varying nature of the power levels attainable from the physical energy sources in aircraft, as well as the above estimated needed power levels for an acoustic-based SHM sensor node with the coupled data elaboration and transmission modules, which could very well reach several hundred mW, a careful investigation of the available EH techniques and their applicability to the case considered herein has to be made.…”
Section: Introductionmentioning
confidence: 99%
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“…In order to harvest energy from FSI using PZT, two types of galloping mechanisms can be used: transverse galloping [91,[152][153][154][155] and wake galloping [91,156,157], as shown in Figures 11 and 12, respectively. The PZT patch is attached on the fixed end of an elastic cantilever beam with an external circuit from which it can be shocked with variable resistance.…”
Section: Galloping-based Pehmentioning
confidence: 99%
“…Detailed reviews on numerous studies of the piezoaeroelastic energy harvesting are given [7,8,[31][32][33]. Although significant attention was given to the piezoaeroelastic energy harvesting, the lack of study on a more practical aerodynamic loading is concerned [8].…”
Section: Introductionmentioning
confidence: 99%