首页> 美国政府科技报告 >Comparisons Between Analogical and Numerical Methods for Studying the Response of an Aircraft to Gusts . Confronti Fra Metodi Analogici E Numerici Per Lo Studio Della Risposta di UN Velivolo Alla Raffica
【24h】

Comparisons Between Analogical and Numerical Methods for Studying the Response of an Aircraft to Gusts . Confronti Fra Metodi Analogici E Numerici Per Lo Studio Della Risposta di UN Velivolo Alla Raffica

机译:用于研究飞机对阵风响应的类比法和数值法的比较。 Confronti Fra metodi analogici E Numerici per Lo studio Della Risposta di UN Velivolo alla Raffica

获取原文

摘要

Two mathematical models for representing nonstationary aerodynamic characteristics of a wing subjected to sharp variations in the angle of attack are used to study the response of an airfoil to ascending vertical gusts. Considering the airfoil to be a rigid body with two degrees of freedom, the flow over the wing in the horizontal plane of the tail and the drag encountered by the tail are calculated. The results obtained using analog and numerical methods are compared.

著录项

  • 作者

    Puccinelli, L.;

  • 作者单位
  • 年度 1970
  • 页码 1-16
  • 总页数 16
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
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