The Aerodynamics of Rapid Area Change in Perching Manoeuvres
atmire.migration.oldid | 2982 | |
dc.contributor.advisor | Rival, David | |
dc.contributor.advisor | Wood, David | |
dc.contributor.author | Polet, Delyle | |
dc.date.accessioned | 2015-02-02T22:31:47Z | |
dc.date.available | 2015-06-23T07:00:40Z | |
dc.date.issued | 2015-02-02 | |
dc.date.submitted | 2015 | en |
dc.description.abstract | This thesis presents a multidisciplinary study on bird perching to inspire Micro Aerial Vehicle design. Birds use a rapid pitch-up manoeuvre during perching, which modifies frontal area. Vorticity fields and forces are measured and simulated on an airfoil performing simultaneous deceleration and pitching to high angles of attack. Forces scale with the shape change number, a ratio between velocity of frontal area change and velocity change during deceleration. A simple analytical model agrees remarkably well with observed forces, and shows that the majority of forces are caused by boundary-layer separation and added-mass effects. Next, the kinematics of a small perching bird (the black-capped chickadee; Poecile atricapillus) are measured and parameterized with a three-dimensional analogue to the two-dimensional shape change number. The shape change numbers used by these birds are within the range of laboratory and computational tests discussed herein. These small birds use shape change numbers in proportion to the kinetic and potential energy at the start of the deceleration phase, in accordance with analytical predictions. | en_US |
dc.identifier.citation | Polet, D. (2015). The Aerodynamics of Rapid Area Change in Perching Manoeuvres (Master's thesis, University of Calgary, Calgary, Canada). Retrieved from https://prism.ucalgary.ca. doi:10.11575/PRISM/28007 | en_US |
dc.identifier.doi | http://dx.doi.org/10.11575/PRISM/28007 | |
dc.identifier.uri | http://hdl.handle.net/11023/2050 | |
dc.language.iso | eng | |
dc.publisher.faculty | Graduate Studies | |
dc.publisher.institution | University of Calgary | en |
dc.publisher.place | Calgary | en |
dc.rights | University of Calgary graduate students retain copyright ownership and moral rights for their thesis. You may use this material in any way that is permitted by the Copyright Act or through licensing that has been assigned to the document. For uses that are not allowable under copyright legislation or licensing, you are required to seek permission. | |
dc.subject | Fluid and Plasma | |
dc.subject | Engineering--Mechanical | |
dc.subject.classification | Biomimicry | en_US |
dc.subject.classification | Unsteady Fluid Dynamics | en_US |
dc.subject.classification | Perching | en_US |
dc.subject.classification | Bird Flight | en_US |
dc.subject.classification | Rapid Area Change | en_US |
dc.subject.classification | 3D Kinematics | en_US |
dc.title | The Aerodynamics of Rapid Area Change in Perching Manoeuvres | |
dc.type | master thesis | |
thesis.degree.discipline | Mechanical and Manufacturing Engineering | |
thesis.degree.grantor | University of Calgary | |
thesis.degree.name | Master of Science (MSc) | |
ucalgary.item.requestcopy | true |
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