...
  • 主题
高级搜索  >
历史搜索 清空历史
首页> 外文期刊>Aerospace science and technology >Aerodynamics and flight mechanics of MAV based on Coanda effect
【24h】

Aerodynamics and flight mechanics of MAV based on Coanda effect

机译：基于柯恩达效应的无人机飞行动力学和飞行力学

获取原文
获取原文并翻译 | 示例
           
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

With the progress and development of Coanda Micro Air Vehicle (MAV) to date, various configurations have been proposed and developed. For the purpose of designing a Micro Air Vehicle (MAV), that could meet the desired mission and design requirements and can operate effectively in various environmental conditions, a workable theoretical analysis is to be developed. With such motivation, capitalizing on the basic fundamental principles, the aerodynamic forces acting on Coanda MAV configurations are revisited and analysed on the bases of the Fluid Dynamics and Flight Mechanics of a semi-spherical Coanda MAV configuration. The major objective of this paper is to analyse the forces and moments acting on the Coanda MAV as related to the geometry, flow, and motion parameters, using mathematical modelling. The mathematical model and derived performance measures in hover and translatory motion are shown to be capable in describing the physical phenomena of the flow field of the semi-spherical Coanda MAV. Results obtained are assessed and considered viable for preliminary design of such air vehicles and further elaborated development, including more flight dynamic manoeuvres. (C) 2016 Elsevier Masson SAS. All rights reserved.
机译：迄今为止，随着柯恩达微型飞行器（MAV）的进步和发展，已经提出并开发了各种配置。为了设计能够满足期望的任务和设计要求并且可以在各种环境条件下有效运行的微型飞行器（MAV），将开发可行的理论分析。借助这种动机，利用基本的基本原理，重新研究了作用于柯恩达MAV构型的空气动力，并基于半球形柯恩达MAV构型的流体动力学和飞行力学进行了分析。本文的主要目的是使用数学模型来分析作用于柯恩达MAV的力和力矩，这些力和力矩与几何，流量和运动参数有关。悬停和平移运动的数学模型和派生的性能度量显示出能够描述半球形柯恩达MAV流场的物理现象。评估所获得的结果，并认为对于此类飞行器的初步设计和进一步完善的开发（包括更多的飞行动态操作）是可行的。 （C）2016 Elsevier Masson SAS。版权所有。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

  • 客服微信

  • 服务号