NASA-TN-D-995-1962 Aerodynamic oads on an Isolated shrouded-propeller configuration for angles of attack from -10 deg to 110 deg《攻角为-10至110的单独遮蔽螺旋桨结构的空气动力学oads》.pdf

《NASA-TN-D-995-1962 Aerodynamic oads on an Isolated shrouded-propeller configuration for angles of attack from -10 deg to 110 deg《攻角为-10至110的单独遮蔽螺旋桨结构的空气动力学oads》.pdf》由会员分享，可在线阅读，更多相关《NASA-TN-D-995-1962 Aerodynamic oads on an Isolated shrouded-propeller configuration for angles of attack from -10 deg to 110 deg《攻角为-10至110的单独遮蔽螺旋桨结构的空气动力学oads》.pdf（32页珍藏版）》请在麦多课文档分享上搜索。

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8、 o0,4 _ 0_ m0 _o %,-Io !r-Io i1)Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-28v,.p0- 0 .090A /64_.29Bv 4010 595. + -+. _70 80 90 I00il(a) Modified-lip configuration.Tp-.7._-_. +-.6 . _- I3 . _i12I .-iI _ _ - _ _-_- _ _- +-+ _ -_+_I0 20 50 _ 60 -8_a, deglio 0o ,128.18.9_. ,268.3 710 .595(b) Original-lip configuration.Figure IP._ Variation of the ratio of propeller thrust to total thrustwlth angle of attack.IProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-