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020 ▼a 9780438353800
035 ▼a (MiAaPQ)AAI10843393
035 ▼a (MiAaPQ)umn:19492
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 247004
0820 ▼a 629.1
1001 ▼a Grover, Maninder S.
24510 ▼a Direct Molecular Simulation of Nitrogen and Oxygen at Hypersonic Conditions.
260 ▼a [S.l.]: ▼b University of Minnesota., ▼c 2018.
260 1 ▼a Ann Arbor: ▼b ProQuest Dissertations & Theses, ▼c 2018.
300 ▼a 169 p.
500 ▼a Source: Dissertation Abstracts International, Volume: 80-01(E), Section: B.
500 ▼a Adviser: Thomas E. Schwartzentruber.
5021 ▼a Thesis (Ph.D.)--University of Minnesota, 2018.
520 ▼a The objective of this thesis is to characterize the gas-phase thermochemical non-equilibrium that occurs during hypersonic flight for nitrogen and oxygen gases.
520 ▼a This thesis uses the direct molecular simulation (DMS) method in conjunction with potential energy surfaces (PESs) to provide an in-depth molecular level analysis of internal energy excitation and dissociation of molecular nitrogen due to N2+N2
520 ▼a The DMS method is used to calculate benchmark data for vibrational energy excitation and non-equilibrium dissociation due to O 2+O interactions. O2+ O interactions are modeled using nine PESs corresponding to. 1 1A', 21A', 1 1A'', 13A', 2 3A', 1
520 ▼a Finally, this thesis explores internal energy exchange processes in oxygen and nitrogen. Probability distribution functions for vibrational energy change during collisions are presented (due to N2+ N2 non-reactive collisions, N2+ N2 exchange rea
590 ▼a School code: 0130.
650 4 ▼a Aerospace engineering.
690 ▼a 0538
71020 ▼a University of Minnesota. ▼b Aerospace Engineering and Mechanics.
7730 ▼t Dissertation Abstracts International ▼g 80-01B(E).
773 ▼t Dissertation Abstract International
790 ▼a 0130
791 ▼a Ph.D.
792 ▼a 2018
793 ▼a English
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T14999928 ▼n KERIS ▼z 이 자료의 원문은 한국교육학술정보원에서 제공합니다.
980 ▼a 201812 ▼f 2019
990 ▼a ***1012033