首页> 美国政府科技报告 >A Comparative Study of Two Computational Methods for Calculating Unsteady Transonic Flows About Oscillating Airfoils.
【24h】

A Comparative Study of Two Computational Methods for Calculating Unsteady Transonic Flows About Oscillating Airfoils.

机译:两种计算摆动翼型非定常跨声速流动计算方法的比较研究。

获取原文

摘要

This report provides a direct comparison of the calculations for the flow field about an oscillating airfoil in a transonic freestream predicted by two computational methods; namely, harmonic analysis and time integration. Details of the two methods are summarized and results for NACA64A010 airfoil oscillating in pitch are considered. Comparisons of the unsteady pressure distribution and resultant lift are presented for several values of free-stream Mach number, angle of attack, and reduced frequency of oscillation. (Author)

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