首页> 美国政府科技报告 >Experimentally determined effects of varying pitch and control stiffnesses on the flutter characteristics at supersonic speeds of all- movable wing and tail models
【24h】

Experimentally determined effects of varying pitch and control stiffnesses on the flutter characteristics at supersonic speeds of all- movable wing and tail models

机译:在所有可移动的机翼和尾翼模型的超音速下,实验确定不同俯仰和控制刚度对颤振特性的影响

获取原文

摘要

Pitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and horizontal tails on fighter aircraft at supersonic speeds

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