ESDU 85010 A-2014
亚音速下完整飞机的侧向力 偏航力矩和滚转力矩导数的估计

Estimation of sideforce@ yawing momentand rolling moment derivatives dueto rate of roll for complete aircraftat subsonic speeds

非常抱歉，我们暂时无法提供预览，您可以试试： 免费下载 ESDU 85010 A-2014 前三页，或者稍后再访问。

您也可以尝试购买此标准，
点击右侧 “购买” 按钮开始采购（由第三方提供）。

注意： 点击下载后，生成下载文件时间比较长，请耐心等待......

标准号

ESDU 85010 A-2014

发布

2014年

发布单位

ESDU - Engineering Sciences Data Unit

当前最新

ESDU 85010 A-2014

 

 

适用范围

ESDU 85010 discusses the application to the complete aeroplane of the prediction methods given in the Series for the contributions to the derivatives from wing planform and dihedral@ and empennage. Illustrations show for diverse configurations at cruise the relative magnitudes of the contributions for each derivative@ and comparisons with experimental data also show the effect of Mach number@ incidence@ wing sweep@ and high lift devices. A detailed comparison of predictions with experimental data drawn from a wide range of sources including tunnel and flight results shows that the sideforce derivative is predicted to within 0.06@ the yawing moment derivative to within 0.016@ and the rolling moment derivative to within 10 per cent. A comprehensive worked example shows the application of the methods. A computer program of the method is provided as ESDUpac A8510.

ESDU 85010 A-2014相似标准

推荐