Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance (1933)
NASA Technical Reports Server (NTRS) · leaf 18
i Change in pitching-moment coefficient, ACL, l i i I i "3 I-"- 3 <s P i— CD CD i 00 r+- n ra O p §-§ 3 «l n fll hi. P 3 " i. to "rT o 5- _ n n ET" 2 3 3 o >-> Ik 3 ra C 1-4- a 8 1 a- a a
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
