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020 ▼a 9780438284319
035 ▼a (MiAaPQ)AAI10969941
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 248032
0820 ▼a 629.1
1001 ▼a Stewart, William John.
24510 ▼a Passive FloodableWing Development for Hybrid Aerial-Aquatic Vehicles.
260 ▼a [S.l.] : ▼b North Carolina State University., ▼c 2018
260 1 ▼a Ann Arbor : ▼b ProQuest Dissertations & Theses, ▼c 2018
300 ▼a 103 p.
500 ▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B.
500 ▼a Adviser: Kara Peters.
5021 ▼a Thesis (Ph.D.)--North Carolina State University, 2018.
520 ▼a Recent interests in hybrid aerial-submersible vehicle technology has led to the development of many such vehicles. Current fully-functional designs consist of either multirotor vehicles or micro air vehicles. As a result of buoyancy challenges s
520 ▼a This work first demonstrated the feasibility of the floodable wing design and Eagleray vehicle concept as a potential solution to the challenges of submerging high volume wings. To demonstrate viability, three conditions were defined. The first
520 ▼a Having demonstrated that the passively flooding and draining wing concept is a viable solution, attention was turned to deriving and experimentally validating a mathematical dynamic model to predict draining performance that is general to any fl
520 ▼a The final research objective was to characterize the aerodynamic drawbacks that result from the design features implemented to enable wing flooding and draining. This was done experimentally by measuring lift and drag of 3D printed models in a w
590 ▼a School code: 0155.
650 4 ▼a Aerospace engineering.
690 ▼a 0538
71020 ▼a North Carolina State University. ▼b Aerospace Engineering.
7730 ▼t Dissertation Abstracts International ▼g 79-12B(E).
773 ▼t Dissertation Abstract International
790 ▼a 0155
791 ▼a Ph.D.
792 ▼a 2018
793 ▼a English
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T15001301 ▼n KERIS
980 ▼a 201812 ▼f 2019
990 ▼a 관리자