An Approach to Integrated Design, Analysis and Data Management for Rapid Air Vehicle Design
An integrated system based on the fusion of proven legacy system and modern PIDO technology has been developed for aircraft configuration development in conceptual and preliminary design phase of aircraft development. KAI-RAVSIM proved successfully the feasibility of new integrated configuration development system by reducing design cycle time and enhancing the design capability. KAI-RAVSIM is currently expanding to be utilized with simulation data management system.
Unable to display preview. Download preview PDF.
- .J.H. Kim, H.H. Jung, Y.H.Lee, S.K.Kim, C.H.Shon, J.H.Seo. and J.H.Shim:KAI-RAVSIM Proof of Concept, 2007 KSAS fall conference, Jeju, Korea, (2007)Google Scholar
- .J.H. Kim, :An Integrated Approach to Aircraft Configuration Development Process, 2008 European Symposium and Seminar Series, Engineous, Munich, Germany, April 14–15, (2008).Google Scholar
- .O. Weck, J. Agte., J. S. Sobieski, P. Arendsen, A. Morris, and M. Spieck, “Sate-of-the-Art and Future Trends in Multidisciplinary Design Optimization”, AIAA 2007-1905Google Scholar
- .K.G. Bowcutt, “A Perspective on the Future of Aerospace Vehicle Design”, AIAA 2003-69Google Scholar