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020 ▼a 9780438075696
035 ▼a (MiAaPQ)AAI10791419
035 ▼a (MiAaPQ)iastate:17343
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 247004
0820 ▼a 629.1
1001 ▼a Ning, Zhe. ▼0 (orcid)0000-0002-4884-5251.
24510 ▼a Experimental Investigations on the Aerodynamic and Aeroacoustic Characteristics of Small UAS Propellers.
260 ▼a [S.l.]: ▼b Iowa State University., ▼c 2018.
260 1 ▼a Ann Arbor: ▼b ProQuest Dissertations & Theses, ▼c 2018.
300 ▼a 167 p.
500 ▼a Source: Dissertation Abstracts International, Volume: 79-11(E), Section: B.
500 ▼a Adviser: Hui Hu.
5021 ▼a Thesis (Ph.D.)--Iowa State University, 2018.
520 ▼a Unmanned aerial system (UAS) is a hot topic in both industry and academia fields. As a popular planform, the rotary-wing system gains more attentions. The small UAS propeller is the most important component in this system, which transfers electr
520 ▼a In the present work, several experimental studies have been performed to investigate the aerodynamic and aeroacoustic characteristics of small UAS propellers. First of all, by conducting force and flow filed measurements, the unsteady dynamic th
520 ▼a During these experimental studies, the force measurements were achieved by a high sensitive force and moment transducer (JR3 load cell), which had a precision of +/-0.1N (+/- 0.25% of the full range). The sound measurements were conducted inside
590 ▼a School code: 0097.
650 4 ▼a Aerospace engineering.
690 ▼a 0538
71020 ▼a Iowa State University. ▼b Aerospace Engineering.
7730 ▼t Dissertation Abstracts International ▼g 79-11B(E).
773 ▼t Dissertation Abstract International
790 ▼a 0097
791 ▼a Ph.D.
792 ▼a 2018
793 ▼a English
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T14997643 ▼n KERIS ▼z 이 자료의 원문은 한국교육학술정보원에서 제공합니다.
980 ▼a 201812 ▼f 2019
990 ▼a ***1012033