...
首页> 外文期刊>Journal of Aircraft >Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summary
【24h】

Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summary

机译:北约航空器的稳定性和控制预测方法的扩展评估:摘要

获取原文
获取原文并翻译 | 示例
           

摘要

This paper presents cross comparisons and assessments of the aerodynamic results obtained within the North Atlantic Treaty Organization's Science and Technology Organisation Applied Vehicle Technology-201 Task Group. The results of five participating organizations and six different computational fluid dynamics solvers are compared to the available wind-tunnel data from the German-Dutch Wind Tunnels, and the results were obtained at low subsonic speeds for both static and dynamic cases. The comparisons help to find commonalities and disparities in the computational fluid dynamics predictions of the aerodynamics of a generic unmanned combat aerial vehicle (the stability and control configuration) and point to areas where computational fluid dynamics is challenged by nonlinear aerodynamics flow prediction. These comparisons help to show where the modeling and simulation of novel aircraft platforms in the earliest stages of design development can contribute to a more successful design process by determining difficult nonlinear aerodynamics and helping to change the design before the later stages of the design process.
机译:本文介绍了在北大西洋公约组织科学技术组织应用车辆技术201任务组中获得的空气动力学结果的交叉比较和评估。将五个参与组织和六个不同的计算流体动力学求解器的结果与德国-荷兰风洞的可用风洞数据进行比较,并且在静态和动态情况下均以低亚音速获得了结果。这些比较有助于发现通用无人驾驶飞行器的空气动力学计算流体动力学预测(稳定性和控制配置)的共性和差异,并指出非线性空气动力学流量预测对计算流体动力学提出挑战的领域。这些比较有助于显示在设计开发的最早阶段,新型飞机平台的建模和仿真可以通过确定困难的非线性空气动力学并有助于在设计过程的后期进行更改来促进更成功的设计过程。

著录项

  • 来源
    《Journal of Aircraft》 |2018年第2期|623-637|共15页
  • 作者单位

    US Air Force Acad, Dept Aeronaut, Colorado Springs, CO 80840 USA;

    US Air Force Acad, Dept Aeronaut, Aeronaut, Colorado Springs, CO 80840 USA;

    German Aerosp Ctr, DLR, Inst Aerodynam & Flow Technol, Brunswick, ME 38108 USA;

    German Aerosp Ctr, DLR, Inst Aerodynam & Flow Technol, Brunswick, ME 38108 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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