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  19 