期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2015
卷号：4
期号：11
页码：10512
DOI：10.15680/IJIRSET.2015.0411025
出版社：S&S Publications
摘要：To find an optimal design solution for Blended Wing Aircraft with desired geometrical model by usingMDO framework . The optimization is carried out in two disciplines viz.., aerodynamics and propulsion. The Range,Aspect ratio and Cruise Thrust of the aircraft are expected to be maximised and the maximum Specific FuelConsumption is expected to be minimised with in the given constraints.The mode FRONTIER is a MDO framework that serves as a platform for the optimization process. The optimizationframework mode FRONTIER is multidisciplinary and multi-objective software written to allow easy coupling to anycomputer aided engineering (CAE) tool is used in optimization process where it represents the set of best solutionspossible.
