NAVWBPS OO-BOT-BO 
APPLICATION OF AERODYNAMlCS 
TO SPECIFIC PROBLEMS OF FLYING 
LIFT DISTRIBUTION 
LBWFT OF SPAN 
TIP VORTEX 
PLANE OF 
SYMMETRY 
REDUCED CHANGE IN 
LIFT DISTRIBUTION 
- 
-- 
%SH 
\’ 
DOCASH 
11 
TRIM CHANGE 
figure 6.10. Interference 8etween Airplanes in Flight