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)
NASA Technical Reports Server (NTRS) · leaf 10
SPINNING CHARACTERISTICS OF THE XN2Y-1 AIRPLANE … Angfe of attack, ct, deg. Angle of attack, cL , deg. T k\ r k1 M I k .08\-& ■ 23° 4lup,4Q°with spin, with spin -25od'n.,40oog'nsf., " , tf" .08 • I I 0°, | | | 0 □ -23° 41 'up, 40 °with spinjf- .04^° 6a-0°. | I sp'h,y' -23°4rup,40°with .-^H .04 ,VJ $ _ 0 68 72 "44 52 56 60 Angle of attack, ct ,…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
