| LDR | | 00000nam u2200205 4500 |
| 001 | | 000000434680 |
| 005 | | 20200226165455 |
| 008 | | 200131s2019 ||||||||||||||||| ||eng d |
| 020 | |
▼a 9781687955555 |
| 035 | |
▼a (MiAaPQ)AAI22621467 |
| 040 | |
▼a MiAaPQ
▼c MiAaPQ
▼d 247004 |
| 082 | 0 |
▼a 621 |
| 100 | 1 |
▼a Hovik, Stefan P. |
| 245 | 10 |
▼a Experimental and Numerical Methods for Characterization of Impact Damage in Titanium-graphite Laminates. |
| 260 | |
▼a [S.l.]:
▼b University of Washington.,
▼c 2019. |
| 260 | 1 |
▼a Ann Arbor:
▼b ProQuest Dissertations & Theses,
▼c 2019. |
| 300 | |
▼a 258 p. |
| 500 | |
▼a Source: Dissertations Abstracts International, Volume: 81-04, Section: B. |
| 500 | |
▼a Advisor: Mamidala, Ramulu. |
| 502 | 1 |
▼a Thesis (Ph.D.)--University of Washington, 2019. |
| 506 | |
▼a This item must not be sold to any third party vendors. |
| 506 | |
▼a This item must not be added to any third party search indexes. |
| 520 | |
▼a TiGr (Titanium-Graphite) is a relatively new aerospace material system composed of layers of titanium alloy and graphite-reinforced thermoplastic. This material is in a class of materials called FMLs (Fiber-Metal-Laminates) which are characterized by high stiffness, fatigue resistance, and strength-to-weight ratios when compared to traditional composites. One of the particularly advantageous properties of TiGr is its damage tolerance |
| 590 | |
▼a School code: 0250. |
| 650 | 4 |
▼a Mechanical engineering. |
| 690 | |
▼a 0548 |
| 710 | 20 |
▼a University of Washington.
▼b Mechanical Engineering. |
| 773 | 0 |
▼t Dissertations Abstracts International
▼g 81-04B. |
| 773 | |
▼t Dissertation Abstract International |
| 790 | |
▼a 0250 |
| 791 | |
▼a Ph.D. |
| 792 | |
▼a 2019 |
| 793 | |
▼a English |
| 856 | 40 |
▼u http://www.riss.kr/pdu/ddodLink.do?id=T15493814
▼n KERIS
▼z 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
| 980 | |
▼a 202002
▼f 2020 |
| 990 | |
▼a ***1008102 |
| 991 | |
▼a E-BOOK |