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INNOVATIVE NOSE CONE DESIGN OF AIRCRAFT

机译:飞机创新的鼻锥设计

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摘要

The term aerodynamic design means to have a drag reducing shape that cause to reduce the resistance offered by the fluid. Currently designs of the aircraft nosecone is simple rigid shaped Our concept is to have a type of inter-flight convertible nosecone, which can change its shape according with the physical condition of the environment, it means when the aircraft is to take-off, at that time it must have the most aerodynamic shape. And thus the shape of its nosecone should be sharp or may be pin pointed. And if the aircraft has to land back on the runway, it has to resist the air so that the landing can be much smoother & safer. Thus the shape of the nosecone must be blunt. To make this possible we have an idea of conversion of the nosecone during the flight, To verify our idea and to found its real application, we have done various aerodynamic nosecone analysis for aircraft, for which we have followed various mathematical series like ogive series, hack series, power series and ellipse series to find out the best possible solution. We are aiming for the better nosecone design of aircraft, whose shape will vary with the situation and thus it is possible to increase the efficiency of the aircraft in terms of aerodynamic.
机译:术语“空气动力学设计”是指具有减阻形状,导致减小流体提供的阻力。当前飞机机头鼻的设计​​是简单的刚性形状我们的概念是拥有一种飞行中的可转换机头鼻翼,可以根据环境的物理条件改变其形状,这意味着飞机何时起飞,那时它必须具有最空气动力学的形状。因此,其鼻锥的形状应该是尖锐的或可以是尖的。而且,如果飞机必须降落在跑道上,则必须抵抗空气,这样降落会更加顺畅和安全。因此,鼻锥的形状必须是钝的。为了使之成为可能,我们有一个在飞行过程中转换鼻锥的想法,为验证我们的想法并找到其实际应用,我们对飞机进行了多种空气动力学鼻锥分析,为此我们遵循了ogive系列等各种数学序列, hack系列,power系列和椭圆系列,以找出最佳的解决方案。我们的目标是更好地设计飞机的鼻锥设计,其形状会随情况而变化,因此有可能在空气动力学方面提高飞机的效率。

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