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020 ▼a 9780438058392
035 ▼a (MiAaPQ)AAI10814268
035 ▼a (MiAaPQ)lehigh:11934
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 248032
0820 ▼a 621
1001 ▼a Fishman, Gregory.
24514 ▼a The Structure of a Perturbed Vortex and Its Interaction with a Wing.
260 ▼a [S.l.] : ▼b Lehigh University., ▼c 2018
260 1 ▼a Ann Arbor : ▼b ProQuest Dissertations & Theses, ▼c 2018
300 ▼a 214 p.
500 ▼a Source: Dissertation Abstracts International, Volume: 79-10(E), Section: B.
500 ▼a Adviser: Donald Rockwell.
5021 ▼a Thesis (Ph.D.)--Lehigh University, 2018.
520 ▼a The study of wingtip vortices and their evolution has been an important topic due to the wide range of applications where they occur. In the present investigation, the evolution of a vortex from an oscillating wing, as well as its subsequent int
520 ▼a The evolution of the vortex from an oscillating wing undergoing small amplitude perturbations shows large fluctuations of axial velocity deficit and circulation during the oscillation cycle. Correspondingly, large variations of swirl ratio occur
520 ▼a The onset and development of orbital motion of a trailing vortex from an oscillating wing has also been characterized
520 ▼a Additionally, large time-dependent variations of the flow structure of the perturbed trailing vortex that impinges upon and develops along a flat plate located downstream are evident, relative to a steady vortex-wing interaction. The nature of t
590 ▼a School code: 0105.
650 4 ▼a Mechanical engineering.
650 4 ▼a Aerospace engineering.
690 ▼a 0548
690 ▼a 0538
71020 ▼a Lehigh University. ▼b Mechanical Engineering.
7730 ▼t Dissertation Abstracts International ▼g 79-10B(E).
773 ▼t Dissertation Abstract International
790 ▼a 0105
791 ▼a Ph.D.
792 ▼a 2018
793 ▼a English
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T14998114 ▼n KERIS
980 ▼a 201812 ▼f 2019
990 ▼a 관리자