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Aircraft Design Parameters Research, Integration And Management Techniques

Posted on:2007-02-15Degree:MasterType:Thesis
Country:ChinaCandidate:H P WangFull Text:PDF
GTID:2192360182479000Subject:Aircraft design
Abstract/Summary:PDF Full Text Request
The Aircraft Conceptual Design is a whole design process. It proceeds from Conceptual Design phase to Preliminary Design Phase with the purpose of offering a optimal aircraft project. Many aircraft primary parameters are involved in this process, The process of determining aircraft parameters is very intricate. It needs experience and iteration. So it costs a lot of time.If a suit of design software has been developed, not only the weary calculation and the iteration can be avoided, but also one or several preliminary concept meeting the design requirements can be brought forward in a short time. With the cycle of the aircraft design shortened, the cost will be saved. So it is very important to study the software about the General Aircraft Design.The process of general aircraft design is detailedly discussed, and the aircraft primary parameters are particularly analyzed in this paper. Aim at the matter appeared in software system, an effective data management method is proposed. By the way of setting up public data structures in the software system, the problem of transferring data in different graphic user interfaces is solved.
Keywords/Search Tags:Aircraft Conceptual Design, Aircraft primary parameters, Graphic user interface, Data structure
PDF Full Text Request
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