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Please use this identifier to cite or link to this item: https://ptsldigital.ukm.my/jspui/handle/123456789/576830
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dc.contributor.authorAbas M. F (UPM)
dc.contributor.authorAftab S. M. A (UPM)
dc.contributor.authorRafie A. S. M (UPM)
dc.contributor.authorYusoff H (UTM)
dc.contributor.authorAhmad K. A (UPM)
dc.date.accessioned2023-11-06T02:08:15Z-
dc.date.available2023-11-06T02:08:15Z-
dc.identifier.issn0128-7680
dc.identifier.otherukmvital:82500
dc.identifier.urihttps://ptsldigital.ukm.my/jspui/handle/123456789/576830-
dc.descriptionThe purpose of this research is to gain initial knowledge and to predict the sustainability of an all-weather Micro-Aerial-Vehicle (MAV). The observed parameters are: the maximum coefficient of lift, C L and the changes in C L after impact, the fluctuation of CL upon entering simulated rain environment, and length of stability recovery in terms of time and flapping cycle, t and t/T, at flapping frequencies of 8, 16, and 24 Hz, at t/T = 3/8 and 7/8. At 24 Hz, the increase in peak C L value after impact of entering rain environment is 0.59. The average fluctuations in C L occurred when entering the rain environment are 410.263. The stability recovery time recorded is 0.006 seconds. Small birds (especially hummingbirds) have a very high flapping frequency that enables them to efficiently withstand external disturbances caused by nature and to instantly adapt to new environments.
dc.language.isoen
dc.publisherUniversiti Putra Malaysia Press
dc.relation.haspartPertanika Journal
dc.relation.urihttp://www.pertanika.upm.edu.my/regular_issues.php?jtype=2&journal=JST-24-2-7
dc.subjectMembrane wing
dc.subjectFlapping
dc.subjectFlat plate
dc.subjectInter-domain
dc.subjectFlapping stability
dc.subjectSimulated rain
dc.titleFlapping membrane wing: a prediction towards inter-domain flight
dc.typeJournal Article
dc.format.volume24
dc.format.pages439-449
dc.format.issue2
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