Aspek Fisika dalam Perancangan Pesawat Aeromodeling Jenis Delta Wing

Muhammad Zuhdi Ronodirdjo, M. Makhrus, W. Wahyudi
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引用次数: 1

Abstract

The Delta Wing aeromodeling aircraft uses a symmetrical airfoil where the top of the wing is the same as the bottom. The main aspects in the design of the Delta Wing aircraft are center of gravity, the engine thrust, the air resistance, the lift and the weight. Delta Wing aircraft are dominated by jet-engined aircraft with the advantages of high speed and small air resistance. From the design and field trials, it was concluded that the minimum thrust of the Delta Win aircraft must be equal to 2 times the total weight of the aircraft so that the aircraft is able to maneuver vertically, perform looping maneuvers, roll maneuvers and hovering.
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这是Delta翼设计飞机的物理方面
三角翼航空模型飞机使用对称翼型,其中机翼的顶部是相同的底部。三角翼飞机设计的主要方面是重心、发动机推力、空气阻力、升力和重量。三角翼飞机以喷气发动机飞机为主,具有速度快、空气阻力小的优点。从设计和现场试验中得出结论,Delta Win飞机的最小推力必须等于飞机总重量的2倍,这样飞机才能进行垂直机动、盘旋机动、滚转机动和悬停。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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