摘要
本文研究了风洞干扰对ＹＦ１６模型实验数据的影响，特别着重于阻塞效应。结论是：提高大攻角实验数据准确度的关键在于减少和修正由于阻塞效应引起的系统误差。
The effect of wind tunnel interference on experimental data of YF16 model has been investigated,with particular emphasis on blockage effect.The conclusion is that the key to raise the experimental accuracy lies in reducing and correcting the systematic errors due to blockage effect at high angles of attack.
关键词
气动力
测量
风洞干扰
风洞试验
aerodynamic measurement test methods wind tunnel interference flow field performance support interference
