Spinning Characteristics of the XN2Y-1 Airplane Obtained from the Spinning Balance and Compared with Results from the Spinning Tunnel and from Flight Tests (1937)
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SPINNING CHARACTERISTICS OF THE XN2Y-1 AIRPLANE \ 6e\ \ \6} \ \ \ \6a 23°4l'up,40°with spin, wii .08- wiihspin/*- "A— --25odn.,40°agnst, M, 0° x- - — o°, i i o°. i I tj o; "□- — C/ » i | . | I l I ' —2 3° 41 'up, 40°with spin -A— ^ .04- --23°4l'upt40°withy^ |vf O- -.04- .0 «- 8 i .5 - 52 56 60 64… … Figure 7—Variation of rolling-moment coefficient Ci (body axes) with angle of attack. 2061—37 2
NASA Technical Reports Server (NTRS)
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