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008200131s2019 ||||||||||||||||| ||eng d
020 ▼a 9781085709392
035 ▼a (MiAaPQ)AAI13856406
040 ▼a MiAaPQ ▼c MiAaPQ ▼d 247004
0820 ▼a 620
1001 ▼a Stefanovic, Milan.
24510 ▼a On the Structural Design Synthesis of Certifiable Aircraft Engine Pylons.
260 ▼a [S.l.]: ▼b University of Washington., ▼c 2019.
260 1 ▼a Ann Arbor: ▼b ProQuest Dissertations & Theses, ▼c 2019.
300 ▼a 230 p.
500 ▼a Source: Dissertations Abstracts International, Volume: 81-03, Section: B.
500 ▼a Advisor: Livne, Eli.
5021 ▼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 The application of an integrated model based process to the design of the structure of an engine pylon at a level of detail and thoroughness that would meet certification requirements leads to significant time and cost savings as well as resulting structure with high strength to weight ratio.Numerous technological hurdles to rapidly generate design synthesis pylon models have been cleared. Newly created modular automation platform (MAP) paves the path, implementing the multi-level sizing process, to model based design synthesis process for pylon certification driven by gradient based optimization algorithm.The integrated model based process introduced in this work can be further extended to the entire aircraft, allowing for dramatic reductions in non-recurring costs, development times, and operational cost.
590 ▼a School code: 0250.
650 4 ▼a Aerospace engineering.
650 4 ▼a Engineering.
690 ▼a 0538
690 ▼a 0537
71020 ▼a University of Washington. ▼b Aeronautics and Astronautics.
7730 ▼t Dissertations Abstracts International ▼g 81-03B.
773 ▼t Dissertation Abstract International
790 ▼a 0250
791 ▼a Ph.D.
792 ▼a 2019
793 ▼a English
85640 ▼u http://www.riss.kr/pdu/ddodLink.do?id=T15490822 ▼n KERIS ▼z 이 자료의 원문은 한국교육학술정보원에서 제공합니다.
980 ▼a 202002 ▼f 2020
990 ▼a ***1816162
991 ▼a E-BOOK