| LDR | | 01660nam u200397 4500 |
| 001 | | 000000422890 |
| 005 | | 20190215170507 |
| 008 | | 181129s2018 |||||||||||||||||c||eng d |
| 020 | |
▼a 9780438071940 |
| 035 | |
▼a (MiAaPQ)AAI10624648 |
| 035 | |
▼a (MiAaPQ)iastate:16853 |
| 040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 247004 |
| 082 | 0 |
▼a 629.1 |
| 100 | 1 |
▼a Fischels, Matthew Vincent. |
| 245 | 10 |
▼a Development of Methods to Improve the Accuracy and Efficiency of Unsteady Incompressible Flow Simulation. |
| 260 | |
▼a [S.l.]:
▼b Iowa State University.,
▼c 2018. |
| 260 | 1 |
▼a Ann Arbor:
▼b ProQuest Dissertations & Theses,
▼c 2018. |
| 300 | |
▼a 241 p. |
| 500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-10(E), Section: B. |
| 500 | |
▼a Adviser: R. G. Rajagopalan. |
| 502 | 1 |
▼a Thesis (Ph.D.)--Iowa State University, 2018. |
| 520 | |
▼a The runtime of unsteady incompressible flows were reduced through different techniques in the formulation and solution of the governing equations. The implicit Runge-Kutta based IRK-SIMPLER algorithm was developed and compared to the Crank-Nicho |
| 590 | |
▼a School code: 0097. |
| 650 | 4 |
▼a Aerospace engineering. |
| 650 | 4 |
▼a Computational physics. |
| 690 | |
▼a 0538 |
| 690 | |
▼a 0216 |
| 710 | 20 |
▼a Iowa State University.
▼b Aerospace Engineering. |
| 773 | 0 |
▼t Dissertation Abstracts International
▼g 79-10B(E). |
| 773 | |
▼t Dissertation Abstract International |
| 790 | |
▼a 0097 |
| 791 | |
▼a Ph.D. |
| 792 | |
▼a 2018 |
| 793 | |
▼a English |
| 856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T14996661
▼n KERIS
▼z 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
| 980 | |
▼a 201812
▼f 2019 |
| 990 | |
▼a ***1012033 |