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NUMERICAL RESEARCH ON EFFICIENCY PERFORMANCE OF THE PROPULSION SYSTEM FOR AN INNOVATIVE AIRSHIP

机译:创新飞艇推进系统效率性能的数值研究

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The current work deals with the methodology and results for the numerical modeling, research and implementation of an unconventional propulsion system for an airship with an innovative shape. It is a part of a global study (European Project MAAT) that investigates the possibilities of using the cruiser/feeders concept for passengers and cargo transportation.Based on an initial research for the airship shape, aerodynamic features at given altitudes, and the propulsion needs, were analyzed by means of numerical simulations for different flow conditions and propulsion concepts. The propulsion system is a set of air-jets, distributed in a circular row around the airship. The air-jets are working with an ambient air that is sucked/blowned from channels positioned in the upper and bottom sides of the airship body. These jets generate thrust to drive the airship in horizontal direction.The flow is modeled using the RANS equations with an appropriate model for turbulence effects simulation. The environmental conditions are varied in order to be representative of several altitude positions for the airship. Boundary zones that were set are "pressure far field", "mass flow inlet", "wall" and "fluid".Attention is focused on the performance of the air-jets working with high mass flow rates and low jet flow speeds. They should also work in different combinations to ensure the needed thrust and direction of flight.The results provide opportunities for future developments of these propulsion concepts for airships.
机译:目前的工作涉及具有创新形状的飞艇非传统推进系统的数值建模,研究和实施的方法和结果。它是全球研究(欧洲项目MAAT)的一部分,调查使用巡洋舰/饲养者概念的乘客和货物运输的可能性。基于飞艇形状的初步研究,给予海拔高度的空气动力学特征以及推进需求,通过用于不同流动条件和推进概念的数值模拟分析。推进系统是一组空气喷射,分布在飞艇周围的圆形行中。空气喷气机正在使用,环境空气从位于飞艇体的上侧和底侧的通道吸入/吹来。这些喷气机在水平方向上产生推动飞艇的推力。使用RAN方程式模拟流量,具有适当的湍流效果模拟模型。为了代表飞艇的几个高度地位,各种环境条件变化。设置的边界区是“压力远场”,“质量流入口”,“墙”和“流体”。表现出来,集中在高质量流量和低射流流速的空气喷射器的性能上。他们还应该采用不同的组合,以确保所需的推力和飞行方向。结果为飞艇这些推进概念的未来发展提供了机会。

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