| LDR | | 00000nmm u2200205 4500 |
| 001 | | 000000331358 |
| 005 | | 20241115154843 |
| 008 | | 181129s2017 ||| | | | eng d |
| 020 | |
▼a 9780438166417 |
| 035 | |
▼a (MiAaPQ)AAI10906647 |
| 040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 248032 |
| 049 | 1 |
▼f DP |
| 082 | 0 |
▼a 629.1 |
| 100 | 1 |
▼a Jones, Ashley M. |
| 245 | 10 |
▼a Unsteady Circulation Control for High-Performance Low-Noise Aircraft. |
| 260 | |
▼a [S.l.] :
▼b University of Florida.,
▼c 2017 |
| 260 | 1 |
▼a Ann Arbor :
▼b ProQuest Dissertations & Theses,
▼c 2017 |
| 300 | |
▼a 491 p. |
| 500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B. |
| 502 | 1 |
▼a Thesis (Ph.D.)--University of Florida, 2017. |
| 520 | |
▼a 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 |
| 520 | |
▼a This dissertation seeks to assess if an actuator array composed of 58 miniature fluidic actuators installed in a supercritical circulation control airfoil with a 30째 trailing edge flap will improve the lift performance while simultaneously reduc |
| 520 | |
▼a 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. |
| 590 | |
▼a School code: 0070. |
| 650 | 4 |
▼a Aerospace engineering. |
| 690 | |
▼a 0538 |
| 710 | 20 |
▼a University of Florida.
▼b Aerospace Engineering. |
| 773 | 0 |
▼t Dissertation Abstracts International
▼g 79-12B(E). |
| 773 | |
▼t Dissertation Abstract International |
| 790 | |
▼a 0070 |
| 791 | |
▼a Ph.D. |
| 792 | |
▼a 2017 |
| 793 | |
▼a English |
| 856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T15000776
▼n KERIS |
| 980 | |
▼a 201812
▼f 2019 |
| 990 | |
▼a 관리자
▼b 관리자 |