| LDR | | 00000nmm u2200205 4500 |
| 001 | | 000000330846 |
| 005 | | 20241105132554 |
| 008 | | 181129s2018 ||| | | | eng d |
| 020 | |
▼a 9780438126305 |
| 035 | |
▼a (MiAaPQ)AAI10903024 |
| 035 | |
▼a (MiAaPQ)umichrackham:001164 |
| 040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 248032 |
| 049 | 1 |
▼f DP |
| 082 | 0 |
▼a 629.1 |
| 100 | 1 |
▼a Marley, Christopher D. |
| 245 | 10 |
▼a Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. |
| 260 | |
▼a [S.l.] :
▼b University of Michigan.,
▼c 2018 |
| 260 | 1 |
▼a Ann Arbor :
▼b ProQuest Dissertations & Theses,
▼c 2018 |
| 300 | |
▼a 163 p. |
| 500 | |
▼a Source: Dissertation Abstracts International, Volume: 79-12(E), Section: B. |
| 500 | |
▼a Adviser: James F. Driscoll. |
| 502 | 1 |
▼a Thesis (Ph.D.)--University of Michigan, 2018. |
| 520 | |
▼a 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 |
| 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=T15000531
▼n KERIS |
| 980 | |
▼a 201812
▼f 2019 |
| 990 | |
▼a 관리자
▼b 관리자 |