Ma = 0.15,Re=6000000. 升力系数 vs 攻角 阻力系数 vs 攻角
《NACA 0012翼型数据.doc》由会员分享,可在线阅读,更多相关《NACA 0012翼型数据.doc(4页珍藏版)》请在人人文库网上搜索。 NACA 0012 AIRFOILS 1.000000 .001260 .987365 .003019 .967647 .005711 .947188 .008436 .926179 .011167 .904775 .013881 .883095 .016562 .861225 .019198 .839225 .021784 .817136 .024...
NACA 0012翼型数据 NACA0012AIRFOILS 1.000000.001260 .987365.003019 .967647.005711 .947188.008436 .926179.011167 .904775.013881 .883095.016562 .861225.019198 .839225.021784 .817136.024314 .794988.026785 .772800.029195 .750587.031542 .728359.033825 .706124.036041 .683889.038188 .661658.040265...
NACA 0012翼型数据 NACA0012AIRFOILS 1.000000.001260 .987365.003019 .967647.005711 .947188.008436 .926179.011167 .904775.013881 .883095.016562 .861225.019198 .839225.021784 .817136.024314 .794988.026785 .772800.029195 .750587.031542 .728359.033825 .706124.036041 .683889.038188 .661658.040265...
NACA 0012翼型数据.doc,NACA 0012 AIRFOILS 1.000000 .001260 .987365 .003019 .967647 .005711 .947188 .008436 .926179 .011167 .904775 .013881 .883095 .016562 .861225 .019198 .839225 .021784 .817136 .024314 .794988 .026785 .772800 .029195 .750587 .031542 .728
NACA0012坐标数据(ICEM) 101 100 0 0 99.9753 0.0036 0 99.9013 0.0143 0 99.7781 0.0322 0 99.6057 0.0572 0 99.3844 0.0891 0 99.1144 0.128 0 98.7958 0.1737 0 98.4292 0.226 0 98.0147 0.2849 0 97.5528 0.3501 0 97.044 0.4216 0 96.4888 0.499 0 95.8877 0.5822 0 95.2414 0.671 0 94.5503 0.7651 0 ...
NACA0012翼型是垂直轴风力机。6、NACA0012翼型的截面与升力阻力曲线图NACA0012翼型是垂直轴风力机的优选翼型,这里根据美国网站提供的技术资料绘制了翼型截面图与升力曲线图,还有根据技术书籍描绘的升力阻力曲线图,供大家参考。 NACA0012翼型的截面图由于NACA0012是对称翼型,在下图左侧数据表中仅列出了单边的数据,表中c是...
NACA0012实验数据 L上-34-11-26-32-36-39-41-44-43-43-42-41-42-40-39-38.5-38-35 L下-34-111-104-90-87-82-78-72-66-61-56-54-48-47-45-42-41-36 X相对位置Cp上0-0.044440.0333330.4666670.0666670.1333330.100.133333-0.088890.166667-0.155560.2-0.20.266667-0.266670.333333...
NACA0012AIRFOILSNACA0012翼型数据NACA0012AIRFOILS1.000000.001260.987365.003019.967647.005711.947188.008436.926179.011167.904775.013881.883095.016562.861225.019198.839225闷纽庆罕福恼呛锋魁肇讫待孤澜喊炮党油滋狱苛飘昆绸颖哭蝇寡挥蟹窥鹰闽榔裤析雏复咙浅赫廓误挞帜肥瘦鞘滦上赦虏牢气预辰周钻烹慧菲痢木故 ...
NACA0012AIRFOILSNACA0012翼型数据NACA0012AIRFOILS1.000000.001260.987365.003019.967647.005711.947188.008436.926179.011167.904775.013881.883095.0..