2012
DOI: 10.1016/j.apor.2012.01.006
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Flexible Oscillating Duct: An approach to a novel propulsor

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Cited by 2 publications
(7 citation statements)
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“…Assuming given values for 0 0 , , , , , , w B R h V ω ψ the motion of the FEOD is fully determined and equations (III.27),(III.28) and (III.29) can be used for the determination of the time dependent geometry and corresponding grid for the FEOD. In case of chord-wise flexibility the FEOD deforms in a similar manner to that discussed in Politis & Tsarsitalidis (2012).…”
Section: )mentioning
confidence: 95%
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“…Assuming given values for 0 0 , , , , , , w B R h V ω ψ the motion of the FEOD is fully determined and equations (III.27),(III.28) and (III.29) can be used for the determination of the time dependent geometry and corresponding grid for the FEOD. In case of chord-wise flexibility the FEOD deforms in a similar manner to that discussed in Politis & Tsarsitalidis (2012).…”
Section: )mentioning
confidence: 95%
“…In , there was a first attempt to systematically investigate the effect of flapping wing propulsor geometry, on its open water performance using UBEM. By further developing specialized data generation codes, the authors presented further simulations of flapping wings, , of bird flight, Politis & Tsarsitalidis (2010) and of a Flexible Oscillating Duct propulsor, Politis & Tsarsitalidis (2012), .…”
Section: Ii11 Boundary Element Methodsmentioning
confidence: 99%
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