자료유형 | 학위논문 |
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서명/저자사항 | On the Structural Design Synthesis of Certifiable Aircraft Engine Pylons. |
개인저자 | Stefanovic, Milan. |
단체저자명 | University of Washington. Aeronautics and Astronautics. |
발행사항 | [S.l.]: University of Washington., 2019. |
발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2019. |
형태사항 | 230 p. |
기본자료 저록 | Dissertations Abstracts International 81-03B. Dissertation Abstract International |
ISBN | 9781085709392 |
학위논문주기 | Thesis (Ph.D.)--University of Washington, 2019. |
일반주기 |
Source: Dissertations Abstracts International, Volume: 81-03, Section: B.
Advisor: Livne, Eli. |
이용제한사항 | This item must not be sold to any third party vendors.This item must not be added to any third party search indexes. |
요약 | 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. |
일반주제명 | Aerospace engineering. Engineering. |
언어 | 영어 |
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