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http://arks.princeton.edu/ark:/88435/dsp015d86p266m
Full metadata record
DC Field | Value | Language |
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dc.contributor.advisor | Stengel, Robert | - |
dc.contributor.author | Qin, Allen | - |
dc.date.accessioned | 2016-07-13T14:08:16Z | - |
dc.date.available | 2016-07-13T14:08:16Z | - |
dc.date.created | 2016-04-28 | - |
dc.date.issued | 2016-07-13 | - |
dc.identifier.uri | http://arks.princeton.edu/ark:/88435/dsp015d86p266m | - |
dc.description.abstract | A submersible aircraft has a large variety of envisioned applications: environmental research, search-and-rescue, surveillance, military defense, etc. Although there have been some success in submersible rotorcraft designs, no successful fixed-wing designs have been demonstrated. Follow-ing bio-inspiration from aquatic diving birds such as the cormorant, a folding wing mechanism is identified as a solution for the large hydrodynamic drag given by the large wingspan of conventional aircraft. The actuation mechanism utilizes a pair of four-bar linkages to constrain the motion of three primary joints to one, allowing for the full contraction and extension of the wing to be actuated by a single servomotor. The mechanism is supported within a detailed, original submersible fuselage design. Although the full manufacture of the design was not attempted, the folding wing mechanism and its integration with a submersible fuselage was conceptually validated by the physical demonstration of a positive result. | en_US |
dc.format.extent | 64 pages | * |
dc.language.iso | en_US | en_US |
dc.title | Design of a Folding-Wing Submersible Aircraft | en_US |
dc.type | Princeton University Senior Theses | - |
pu.date.classyear | 2016 | en_US |
pu.department | Mechanical and Aerospace Engineering | en_US |
pu.pdf.coverpage | SeniorThesisCoverPage | - |
Appears in Collections: | Mechanical and Aerospace Engineering, 1924-2020 |
Files in This Item:
File | Size | Format | |
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Qin_Allen_Thesis.pdf | 13.61 MB | Adobe PDF | Request a copy |
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