NAWWEPS 00-8OT-80  BASIC AERODYNAMICS  57  NO SEPARATION  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) 