英国论文代写利物浦大学：飞艇设计

英国论文代写利物浦大学：飞艇设计

飞艇有一个集成的电动螺旋桨，可以帮助飞艇在空中进行机动和导航。这种飞艇可分为三种。它是刚性的，半刚性的和非刚性的。有一些特征可以用来划分这三种。已经观察到，对于刚性类型的飞艇，存在用于保持包络形状的内部金属框架。在半刚性飞艇的情况下，存在由刚性龙骨保持的形状，其贯穿封套的长度。非刚性类型具有提升气体的内部压力。这是氦气，它有助于保持包络形状。该项目涉及设计和建造与推进系统集成的太阳能飞艇。在该项目的初始阶段，通过仅考虑与空气动力学特性和稳定性相关的少数变量来解释最佳形状。发现聚酯薄膜材料被提出并建造。

这是耐用且轻便的，用于飞艇的外壳。结果发现，氦气用于测试风洞，以确定封套的最佳形状和扭曲。除此之外，太阳能模块需要动力以确保飞艇的设计符合要求。太阳墩的电压量和电流输出量。根据先前的研究和分析，已经需要太阳能模块的电压和电流输出量来满足电池的额定值。电池一直被认为是飞艇的主要动力源。该电池用于为其他相关组件供电并提供能量。这包括推进和控制系统。该系统设计中的太阳能模块仅用于为电池充电。推进和控制系统对项目至关重要。推进系统用于为飞艇提供漂浮在空中的能力，同时由控制系统控制飞艇。

英国论文代写利物浦大学：飞艇设计

An airship has an integrated motor driven propeller that aid the airship to maneuver and navigate in the air. This airship can be divided into three kinds. It is rigid, semi-rigid and non-rigid. There are some characteristic features that can be used to divide the three kinds. It has been observed that for the rigid kind of airship, there is an internal metal frame that is used to maintain the envelope shape. In the case of semi rigid airship, there is a shape that is maintained by the rigid keels which runs through the length of the envelope. The non-rigid kind has an internal pressure of lifting gas. This is helium and it aids in the maintenance of the envelope shape. The project is about designing and building solar powered airship that is integrated with the propulsion system. During the initial stage of this project, the best shape was construed by considering only a few variables that were related to the aerodynamic characteristic and stability. It was found that the mylar material was proposed and built.
This was durable and lightweight that is used in the envelope of the airship. It was found that the helium gas is used to test the wind tunnel to decide the best shape and contortion for the envelope. Added to this, the solar modules need power to ensure that the airship has been designed as per requirements. The amount of voltage and the current output of the solar mound. According to previous research and analysis, it has been that the amount of voltage and current output of the solar modules is needed to meet the rating of the battery. The battery has been considered as the main power source of the airship. This battery is used to power and provide energy for other related components. This includes propulsion and the control systems. The solar modules in this system design are used to only charge the battery. The propulsion and the control system are critical for the project. The propulsion system is used to provide airship with the ability to float in air, while it is being controlled by the control system.