File:Gliding-Swifts-Attain-Laminar-Flow-over-Rough-Wings-pone.0099901.s003.ogv
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Gliding-Swifts-Attain-Laminar-Flow-over-Rough-Wings-pone.0099901.s003.ogv (Ogg multiplexed audio/video file, Theora/Vorbis, length 1 min 11 s, 640 × 480 pixels, 529 kbps overall, file size: 4.48 MB)
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[edit]DescriptionGliding-Swifts-Attain-Laminar-Flow-over-Rough-Wings-pone.0099901.s003.ogv |
English: Laminar-turbulent transition at maximum lift-drag ratio. Video demonstration of the detection of laminar-turbulent transition with the stethoscope on a fully extended swift wing at 10 ms−1 attaining maximum lift to drag ratio. At some wing sections, a distinct tone can be heard at a frequency of about 1010 Hz. |
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Source | Movie S1 from Lentink D, de Kat R (2014). "Gliding Swifts Attain Laminar Flow over Rough Wings". PLOS ONE. DOI:10.1371/journal.pone.0099901. PMID 24964089. PMC: 4070913. | ||
Author | Lentink D, de Kat R | ||
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![]() ![]() This file is licensed under the Creative Commons Attribution 4.0 International license.
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 05:58, 1 July 2014 | 1 min 11 s, 640 × 480 (4.48 MB) | Open Access Media Importer Bot (talk | contribs) | Automatically uploaded media file from Open Access source. Please report problems or suggestions here. |
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Author | Lentink D, de Kat R |
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Usage terms | http://creativecommons.org/licenses/by/4.0/ |
Image title | Laminar-turbulent transition at maximum lift-drag ratio. Video demonstration of the detection of laminar-turbulent transition with the stethoscope on a fully extended swift wing at 10 ms−1 attaining maximum lift to drag ratio. At some wing sections, a distinct tone can be heard at a frequency of about 1010 Hz. |
Software used | |
Date and time of digitizing | 2014 |
Language | English |