Inside Out Library · Explore
Spinning Characteristics of Wings III : a Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips (1937)
NASA Technical Reports Server (NTRS) · leaf 22
Fig. 7b N.A.C.A. Technical Note No. 612 4 Angle cf attack, of ,deg. Figure 7b.- Variation of normal-force coefficient Oz (body axes) with angle of attack; 5i2 tapered wing, rounded tips.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Spinning Characteristics of Wings III : a Rectangular and Tapered Clark Y Monoplane Wing with Rounded Tips
More like this
