首页> 外国专利> Aerodynamic coefficient's rigid value determining method for aircraft e.g. A320 aircraft, involves determining experimental value of aerodynamic coefficient, and determining rigid value of aerodynamic coefficient

Aerodynamic coefficient's rigid value determining method for aircraft e.g. A320 aircraft, involves determining experimental value of aerodynamic coefficient, and determining rigid value of aerodynamic coefficient

机译:飞机空气动力学系数的刚性值确定方法A320飞机涉及确定空气动力学系数的实验值和确定空气动力学系数的刚性值

摘要

The method involves realizing wind tunnel measurements on aircraft symbol, and determining experimental value i.e. flexible symbol value, of aerodynamic coefficient from the wind tunnel measurements. A rigid value of aerodynamic coefficient is determined from the experimental value and flexible correction factor of symbol, where the rigid value of aerodynamic coefficient is equal to product of the experimental value and the flexible correction factor.
机译:该方法包括在飞机符号上实现风洞测量,并从风洞测量中确定空气动力学系数的实验值,即柔性符号值。空气动力学系数的刚性值由符号的实验值和柔性校正因子确定,其中空气动力学系数的刚性值等于实验值与柔性校正因子的乘积。

著录项

  • 公开/公告号FR2942038A1

    专利类型

  • 公开/公告日2010-08-13

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20090000548

  • 发明设计人 CALMELS BENOIT;

    申请日2009-02-09

  • 分类号G01M9/06;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:36

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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