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Experimental Investigations on the Aerodynamic and Aeroacoustic Characteristics of Small UAS Propellers
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| 자료유형 | 학위논문 |
|---|---|
| 서명/저자사항 | Experimental Investigations on the Aerodynamic and Aeroacoustic Characteristics of Small UAS Propellers. |
| 개인저자 | Ning, Zhe. |
| 단체저자명 | Iowa State University. Aerospace Engineering. |
| 발행사항 | [S.l.]: Iowa State University., 2018. |
| 발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2018. |
| 형태사항 | 167 p. |
| 기본자료 저록 | Dissertation Abstracts International 79-11B(E). Dissertation Abstract International |
| ISBN | 9780438075696 |
| 학위논문주기 | Thesis (Ph.D.)--Iowa State University, 2018. |
| 일반주기 |
Source: Dissertation Abstracts International, Volume: 79-11(E), Section: B.
Adviser: Hui Hu. |
| 요약 | 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 |
| 요약 | 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 |
| 요약 | 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 |
| 일반주제명 | Aerospace engineering. |
| 언어 | 영어 |
| 바로가기 | 
: 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
