LDR | | 02025nmm uu200421 4500 |
001 | | 000000331356 |
005 | | 20240805164224 |
008 | | 181129s2016 |||||||||||||||||c||eng d |
020 | |
▼a 9780438165786 |
035 | |
▼a (MiAaPQ)AAI10906578 |
040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 248032 |
082 | 0 |
▼a 629.1 |
100 | 1 |
▼a DeSouza, Shaun. |
245 | 10 |
▼a Disintegration of Single Orifice and Coaxial Supercritical Jets. |
260 | |
▼a [S.l.] :
▼b University of Florida.,
▼c 2016 |
260 | 1 |
▼a Ann Arbor :
▼b ProQuest Dissertations & Theses,
▼c 2016 |
300 | |
▼a 188 p. |
500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B. |
502 | 1 |
▼a Thesis (Ph.D.)--University of Florida, 2016. |
520 | |
▼a Two separate experimental studies were undertaken to characterize the behavior of single orifice and coaxial supercritical jets injected into environments varying from sub-to supercritical conditions. It was determined that the chamber-to-inject |
520 | |
▼a The study of single orifice jets covered a broad range of density ratios. The data was compared to previous single orifice injection studies performed in the same facility under similar conditions. The jet disintegration process was observed fro |
520 | |
▼a Density distribution was quantified for coaxial jets injected in an inert gaseous atmosphere under a range of subcritical and supercritical conditions. Density gradient profiles were inferred from the experimental data. A novel method was applie |
590 | |
▼a School code: 0070. |
650 | 4 |
▼a Aerospace engineering. |
650 | 4 |
▼a Mechanical engineering. |
650 | 4 |
▼a Engineering. |
690 | |
▼a 0538 |
690 | |
▼a 0548 |
690 | |
▼a 0537 |
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 2016 |
793 | |
▼a English |
856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T15000768
▼n KERIS |
980 | |
▼a 201812
▼f 2019 |
990 | |
▼a 관리자 |