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Direct Molecular Simulation of Nitrogen and Oxygen at Hypersonic Conditions
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| 자료유형 | 학위논문 |
|---|---|
| 서명/저자사항 | Direct Molecular Simulation of Nitrogen and Oxygen at Hypersonic Conditions. |
| 개인저자 | Grover, Maninder S. |
| 단체저자명 | University of Minnesota. Aerospace Engineering and Mechanics. |
| 발행사항 | [S.l.]: University of Minnesota., 2018. |
| 발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2018. |
| 형태사항 | 169 p. |
| 기본자료 저록 | Dissertation Abstracts International 80-01B(E). Dissertation Abstract International |
| ISBN | 9780438353800 |
| 학위논문주기 | Thesis (Ph.D.)--University of Minnesota, 2018. |
| 일반주기 |
Source: Dissertation Abstracts International, Volume: 80-01(E), Section: B.
Adviser: Thomas E. Schwartzentruber. |
| 요약 | The objective of this thesis is to characterize the gas-phase thermochemical non-equilibrium that occurs during hypersonic flight for nitrogen and oxygen gases. |
| 요약 | 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 |
| 요약 | 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 |
| 요약 | 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 |
| 일반주제명 | Aerospace engineering. |
| 언어 | 영어 |
| 바로가기 | 
: 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
