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Integration of Multifidelity Multidisciplinary Computer Codes for Design and Analysis of Supersonic Aircraft

机译:集成多保真多学科计算机代码,用于超音速飞机的设计和分析

摘要

This paper documents the development of a conceptual level integrated process for design and analysis of efficient and environmentally acceptable supersonic aircraft. To overcome the technical challenges to achieve this goal, a conceptual design capability which provides users with the ability to examine the integrated solution between all disciplines and facilitates the application of multidiscipline design, analysis, and optimization on a scale greater than previously achieved, is needed. The described capability is both an interactive design environment as well as a high powered optimization system with a unique blend of low, mixed and high-fidelity engineering tools combined together in the software integration framework, ModelCenter. The various modules are described and capabilities of the system are demonstrated. The current limitations and proposed future enhancements are also discussed.
机译:本文记录了用于设计和分析高效且环保的超音速飞机的概念​​级集成过程的发展。为了克服实现该目标的技术挑战,需要一种概念设计功能,该功能可为用户提供检查所有学科之间的集成解决方案的能力,并以比以前实现的更大的规模促进多学科设计,分析和优化的应用。 。所描述的功能既包括交互式设计环境,也包括功能强大的优化系统,该系统在软件集成框架ModelCenter中将低,混合和高保真度的工程工具进行了独特的混合。描述了各种模块并演示了系统的功能。还讨论了当前的局限性和建议的未来增强功能。

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