LDR | | 00000nmm u2200205 4500 |
001 | | 000000331786 |
005 | | 20241120142447 |
008 | | 181129s2018 ||| | | | eng d |
020 | |
▼a 9780438126732 |
035 | |
▼a (MiAaPQ)AAI10903067 |
035 | |
▼a (MiAaPQ)umichrackham:001275 |
040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 248032 |
049 | 1 |
▼f DP |
082 | 0 |
▼a 629.1 |
100 | 1 |
▼a Fievet, Romain. |
245 | 10 |
▼a Impact of Vibrational Nonequilibrium on the Simulation and Modeling of Dual-Mode Scramjets. |
260 | |
▼a [S.l.] :
▼b University of Michigan.,
▼c 2018 |
260 | 1 |
▼a Ann Arbor :
▼b ProQuest Dissertations & Theses,
▼c 2018 |
300 | |
▼a 317 p. |
500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B. |
500 | |
▼a Adviser: Venkatramanan Raman. |
502 | 1 |
▼a Thesis (Ph.D.)--University of Michigan, 2018. |
520 | |
▼a The practical realization of supersonic flight relies on the development of a robust propulsion system. These air-breathing scramjet engines process fuel and high-speed air to generate propulsive thrust. Unlike conventional jet engines, scramjet |
520 | |
▼a Of particular focus is the role of molecular processes in the development of the shocks. At high enthalpy conditions, the internal motions of the molecules are moved out of equilibrium due to compression shocks, which affects not only the thermo |
520 | |
▼a These studies revealed the following key features: a) nonequilibrium of vibrational states greatly increases pseudoshock length, b) contrary to external hypersonics, nonequilibrium accelerates chemical reactions in the combustor, reducing the di |
590 | |
▼a School code: 0127. |
650 | 4 |
▼a Aerospace engineering. |
690 | |
▼a 0538 |
710 | 20 |
▼a University of Michigan.
▼b Aerospace Engineering. |
773 | 0 |
▼t Dissertation Abstracts International
▼g 79-12B(E). |
773 | |
▼t Dissertation Abstract International |
790 | |
▼a 0127 |
791 | |
▼a Ph.D. |
792 | |
▼a 2018 |
793 | |
▼a English |
856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T15000563
▼n KERIS |
980 | |
▼a 201812
▼f 2019 |
990 | |
▼a 관리자
▼b 관리자 |