| LDR | | 02755nmm uu200409 4500 |
| 001 | | 000000330925 |
| 005 | | 20240805163101 |
| 008 | | 181129s2018 |||||||||||||||||c||eng d |
| 020 | |
▼a 9780438134812 |
| 035 | |
▼a (MiAaPQ)AAI10903656 |
| 040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 248032 |
| 082 | 0 |
▼a 621 |
| 100 | 1 |
▼a Fernandez, Sebastian Ferreyro. |
| 245 | 10 |
▼a Advanced Soot and Radiation Models for Laminar and Turbulent Flames. |
| 260 | |
▼a [S.l.] :
▼b The Pennsylvania State University.,
▼c 2018 |
| 260 | 1 |
▼a Ann Arbor :
▼b ProQuest Dissertations & Theses,
▼c 2018 |
| 300 | |
▼a 160 p. |
| 500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B. |
| 502 | 1 |
▼a Thesis (Ph.D.)--The Pennsylvania State University, 2018. |
| 520 | |
▼a The design strategies for the next generation of low-emission combustion systems are highly focused on reducing pollutant emissions, and designers need to perform numerical simulations that incorporate detailed soot and radiative heat transfer m |
| 520 | |
▼a The three major model implementations included in this work are a laminar flame solver, soot models, and a radiative heat transfer model. The laminar combustion solver can be used in any geometrical configuration of premixed and diffusion flames |
| 520 | |
▼a The laminar flame solver performance is evaluated in two configurations: a freely propagated methane-air premixed flame, and a counter-flow ethylene-air diffusion flame. The premixed flame is used to evaluate the laminar solver and the radiative |
| 520 | |
▼a The effects of turbulence-chemistry interaction in soot and radiative heat transfer are quantified for a transient high-pressure turbulent spray flame. Numerical simulations are carried out using an unsteady Reynolds-averaged Navier-Stokes (RANS |
| 520 | |
▼a Computed liquid and vapor penetration versus time, ignition delay, and flame lift-off height are, for the purposes of the present work, consistent with experimental values. The largest differences appear for flame lift-off, with differences up t |
| 520 | |
▼a The uncoupled PMC/LBL model is used to compute the spectral intensity distribution of the radiation inside the domain and to evaluate the effects of turbulence-radiation interaction (TRI). In these flames, radiative heat transfer represents a sm |
| 590 | |
▼a School code: 0176. |
| 650 | 4 |
▼a Mechanical engineering. |
| 690 | |
▼a 0548 |
| 710 | 20 |
▼a The Pennsylvania State University.
▼b Mechanical Engineering. |
| 773 | 0 |
▼t Dissertation Abstracts International
▼g 79-12B(E). |
| 773 | |
▼t Dissertation Abstract International |
| 790 | |
▼a 0176 |
| 791 | |
▼a Ph.D. |
| 792 | |
▼a 2018 |
| 793 | |
▼a English |
| 856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T15000650
▼n KERIS |
| 980 | |
▼a 201812
▼f 2019 |
| 990 | |
▼a 관리자 |