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Integrated analysis procedure of aerospace composite structure

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dc.contributor.advisor Patrick Hale. en_US
dc.contributor.author Ahn, Junghyun en_US
dc.contributor.other System Design and Management Program. en_US
dc.date.accessioned 2008-11-07T19:03:10Z
dc.date.available 2008-11-07T19:03:10Z
dc.date.copyright 2008 en_US
dc.date.issued 2008 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/43106
dc.description Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, 2008. en_US
dc.description Includes bibliographical references (p. 50). en_US
dc.description.abstract The emergence of composite material application in major commercial aircraft design, represented by the Boeing 787 and Airbus A350-XWB, signals a new era in the aerospace industry. The high stiffness to weight ratio of continuous fiber composites (CFC) makes CFCs one of the most important materials to be introduced in modern aircraft industry. In addition to inherent strength (per given weight) of CFCs, they also offer the unusual opportunity to design the structure and material concurrently. The directional properties (and the ability to change these properties through the design process) of composite materials can be used in aeroelastically tailored wings, the fuselage and other critical areas. Due to the longer lifecycle (25-30 years) of a commercial airliner and the tools and processes developed for the airplane of previous product development cycles, new technology often ends up being deployed less effectively because of the mismatch in the technical potential (what can be done) vs. design tools and processes (what was done before). Tools and processes need to be current to take advantage of latest technology, and this thesis will describe one possible approach in primary composite structural design area using integrated structural analysis en_US
dc.description.statementofresponsibility by Junghyun Ahn. en_US
dc.format.extent 50 p. en_US
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. en_US
dc.rights.uri http://dspace.mit.edu/handle/1721.1/7582 en_US
dc.subject System Design and Management Program. en_US
dc.title Integrated analysis procedure of aerospace composite structure en_US
dc.type Thesis en_US
dc.description.degree S.M. en_US
dc.contributor.department System Design and Management Program. en_US
dc.identifier.oclc 244636729 en_US


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