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Unsteady Circulation Control for High-Performance Low-Noise Aircraft
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| 자료유형 | 학위논문 |
|---|---|
| 서명/저자사항 | Unsteady Circulation Control for High-Performance Low-Noise Aircraft. |
| 개인저자 | Jones, Ashley M. |
| 단체저자명 | University of Florida. Aerospace Engineering. |
| 발행사항 | [S.l.]: University of Florida., 2017. |
| 발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2017. |
| 형태사항 | 491 p. |
| 기본자료 저록 | Dissertation Abstracts International 79-12B(E). Dissertation Abstract International |
| ISBN | 9780438166417 |
| 학위논문주기 | Thesis (Ph.D.)--University of Florida, 2017. |
| 일반주기 |
Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B.
|
| 요약 | With today's increasing population and communities being built closer to airports, there is an increased sensitivity to aircraft noise. Extensive research has been put into reducing aircraft noise over populated areas including jet engine design |
| 요약 | This dissertation seeks to assess if an actuator array composed of 58 miniature fluidic actuators installed in a supercritical circulation control airfoil with a 30° trailing edge flap will improve the lift performance while simultaneously reduc |
| 요약 | The present results represent the first of their kind to assess the effects of unsteady versus steady circulation control on both aerodynamic and aeroacoustic performance of a representative supercritical airfoil. |
| 일반주제명 | Aerospace engineering. |
| 언어 | 영어 |
| 바로가기 | 
: 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
