NAVWEPS GO-BOT-BO 
BASIC AERODYNAMlCS 
BASIC AIRFOIL SHAPE 
AND ANGLE OF ATTACK 
ORIGINAL ANGLE OF ATTACK 
AND DYNAMIC/PRESSURE, 9 
ORIGINAL ANGLE OF ATTACK 
BUT INCREASED DYNAMIC PRESSURE 
ORIGINAL ANGLE OF ATTACK AND DYNAMIC 
PRESSURE BUT ONE-HALF ORIGINAL SIZE 
AIRFOIL SHAPE AND ANGLE OF ATTACK DEFINE 
RELATIVE PRESSURE DISTRIBUTION 
Figure 1.9. Airfoil Pressure Distribution 
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