基于三体船体概念的先进水上飞机概念设计综述

Tech Hamza Ahmad Malik, Khurram Baig, Khizar Ahmad Baqai, Ilyas Mehmood Qureshi, Shoaib Randhawa, Wajeeh Hassan
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引用次数: 0

摘要

1950年后,水上飞机的研究开始下降,当时的重点转向了改善陆基飞机的基础设施。从那时起,现有的设计经过了微小的改进。本文的目标是对一个接一个的参数进行批判性的讨论,在此基础上对水上飞机的特定设计配置进行评估。基于三体船的配置是基于浮动飞机和飞艇的混合。一旦升空,它具有更低的空气动力阻力。流体静力稳定性是由重心高度和重心高度相互作用产生的恢复力矩来实现的。它们通过重心与元中心高度相互作用产生的恢复力矩实现了优越的稳定性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Review on Advance Seaplane Conceptual Design Adapting Trimaran Boat Hull Concept
The decline in the research of seaplanes started after 1950, when the focus shifted towards improving the infrastructure of land-based aircrafts. Existing designs with minor improvements are being used since then. The goal is to critically discuss the parameters one by one based on which a specific design configuration of a seaplane is evaluated in this paper. Trimaran based configuration is based on a blend of float plane and flying boat. It has lower aerodynamic drag once airborne. The hydrostatic stability is achieved by the restoring moment generated by the interaction between cg and mc height. They have superior stability achieved by the restoring moment generated by the interaction between center of gravity and meta center height.
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