Skip navigation
Please use this identifier to cite or link to this item: http://arks.princeton.edu/ark:/88435/dsp01jd472w52n
Full metadata record
DC FieldValueLanguage
dc.contributor.advisorSmits, Alexander Jen_US
dc.contributor.authorDewey, Peteren_US
dc.contributor.otherMechanical and Aerospace Engineering Departmenten_US
dc.date.accessioned2013-05-21T13:34:25Z-
dc.date.available2013-05-21T13:34:25Z-
dc.date.issued2013en_US
dc.identifier.urihttp://arks.princeton.edu/ark:/88435/dsp01jd472w52n-
dc.description.abstractExperiments are conducted to better understand the effects of flexibility in generating unsteady bio-inspired propulsion. It is found that by exploiting the effects of flexibility, the thrust production and propulsive efficiency can be up to twice that of a rigid propulsor. The wakes are highly dependent on the input parameters to the system such as the oscillation frequency and chordwise traveling wave wavelength that develops along a flexible surface. In general, the wakes of flexible propulsors tend to concentrate their momentum in the direction of motion whereas the wakes of rigid propulsors have relatively larger momentum in the transverse direction leading to a decrease in propulsive efficiency. A linear stability analysis is conducted on the wakes to determine the wake resonant frequencies. It is found that when the driving oscillation frequency of the apparatus matches the wake resonant frequency there is a local peak in propulsive efficiency. The global peak in efficiency occurs only when the structural resonant frequency of the flexible structure is coincident with the wake resonant frequency, which only occurs under very specific conditions. This implies that there is an optimum flexibility to maximize propulsive efficiency; being either too stiff or too flexible is detrimental to propulsive performance. Since both the structural resonant frequency and wake resonant frequencies are finite, this also suggests that animals must utilize flexible propulsive surfaces if they are to optimize their efficiencies. Finally, a non-dimensional scaling argument is made that is shown to collapse the thrust production, power input to the fluid, and propulsive efficiency for a range of propulsors with various flexibilities and aspect ratio.en_US
dc.language.isoenen_US
dc.publisherPrinceton, NJ : Princeton Universityen_US
dc.relation.isformatofThe Mudd Manuscript Library retains one bound copy of each dissertation. Search for these copies in the <a href=http://catalog.princeton.edu> library's main catalog </a>en_US
dc.subjectFluid dynamicsen_US
dc.subjectPropulsionen_US
dc.subjectSwimming/Flyingen_US
dc.subjectVortex dynamicsen_US
dc.subject.classificationAerospace engineeringen_US
dc.subject.classificationMechanical engineeringen_US
dc.titleUnderwater Flight: Hydrodynamics of the Manta Rayen_US
dc.typeAcademic dissertations (Ph.D.)en_US
pu.projectgrantnumber690-2143en_US
Appears in Collections:Mechanical and Aerospace Engineering

Files in This Item:
File Description SizeFormat 
Dewey_princeton_0181D_10550.pdf20.73 MBAdobe PDFView/Download


Items in Dataspace are protected by copyright, with all rights reserved, unless otherwise indicated.