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008181129s2018 ||| | | | eng d
020 ▼a 9780438126732
035 ▼a (MiAaPQ)AAI10903067
035 ▼a (MiAaPQ)umichrackham:001275
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 248032
0491 ▼f DP
0820 ▼a 629.1
1001 ▼a Fievet, Romain.
24510 ▼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.
5021 ▼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
71020 ▼a University of Michigan. ▼b Aerospace Engineering.
7730 ▼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
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T15000563 ▼n KERIS
980 ▼a 201812 ▼f 2019
990 ▼a 관리자 ▼b 관리자