NO SEPARATION 
NAWWEPS 00-8OT-80 
BASIC AERODYNAMICS 
SEPARATION 1 
BOUNDARY LAYER 
SEPAF --‘-.’ iAT ION /------- 
SEPARATION AT STALL 
REVERSE 
FLOW 
b SHOCK WAVE 
SHOCK WAVE INDUCED 
FLOW SEPARATION 
Figure 1.26. Airflow Separation (sheet 7 of 2) 
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