一种高亚音速中程喷气客机的设计与性能分析:概念方法

2015 International Conference on Electrical & Electronic Engineering (ICEEE) Pub Date : 2015-11-01 DOI:10.1109/CEEE.2015.7428246

M. Muhammad, M. Arifuzzaman, D. Swarnaker, M. M. Hossain

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引用次数: 0

摘要

介绍了450座节油高亚音速中程客机的概念设计。在这里，首要考虑的是在降低最终燃料成本的情况下运送更多的乘客。飞行性能分析的目的是在任务剖面中允许巡航、爬升和下降部分的柔韧变化。利用仿真技术对多次迭代结果进行数值变换，得到结构分析和气动特性。

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Design and performance analysis of a high-subsonic middle range jetliner: A conceptual approach

This paper represents conceptual design of 450 seated fuel efficient high subsonic middle range passenger aircraft. Here the prime concern is to carry more passengers with reduced ultimate fuel cost. The flight performance analysis is designed to allow pliable variation of cruise, climb and descent segments in the mission profile. Simulation technique is used to find structural analysis and aerodynamic characteristics by numerical transformation of several iteration results.

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2015 International Conference on Electrical & Electronic Engineering (ICEEE)

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