1.6 



1.4 

 1.2 

 1.0 



0.8 

 0.6 

 0.4 

 0.2 

 0.0 



I I I I I I 11 I I I I 11 I I I I l| I I I I I I 1 1 I I I I I I I I I I I^i4 I lAM I I 



SYMBOL 

 O 



D 



■ 



o 



♦ 



^^■(deg) 



-6.0 

 -6.0 

 -7.0 

 -7.0 

 -8.0 

 -8.0 



V(Kt) 



8.0 

 10.0 



8.0 /?£;-, 

 10.0 



8,0 

 10.0 





V\ J 



/ 



<u^ 



I H I I I I I I I I 11 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I 



-25 -20 -15 -10 -5 5 10 15 20 25 



FLAP DEFLECTION, 6 (deg) 



Figure 9 - Depressor Coefficient of Tension as a Function of Control Flap 

 Deflection for Various Speeds and Horizontal Stabilizer 

 Incidence Angles 



22 



