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Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle
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| 자료유형 | 학위논문 |
|---|---|
| 서명/저자사항 | Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. |
| 개인저자 | Marley, Christopher D. |
| 단체저자명 | University of Michigan. Aerospace Engineering. |
| 발행사항 | [S.l.]: University of Michigan., 2018. |
| 발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2018. |
| 형태사항 | 163 p. |
| 기본자료 저록 | Dissertation Abstracts International 79-12B(E). Dissertation Abstract International |
| ISBN | 9780438126305 |
| 학위논문주기 | Thesis (Ph.D.)--University of Michigan, 2018. |
| 일반주기 |
Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B.
Adviser: James F. Driscoll. |
| 요약 | Due to the large aerodynamic heating at high Mach numbers, Thermal Protection System (TPS) design considerations are critical for hypersonic vehicles, and engineers seek to incorporate heating constraints earlier in the design process. Prelimina |
| 일반주제명 | Aerospace engineering. |
| 언어 | 영어 |
| 바로가기 | 
: 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
