NAVWEPS GO-BOT-BO 
STABILITY AND CONTROL 
n f WING.NACELLE,AND FUSELAGE 
MOMENTS AFFECTED BY 
SLIPSTREAM 
-DYNAMIC PRESSURE 
AT TAIL AFFECTED 
BY SLIPSTREAM 
WING LIFT AFFECTED 
BY SLIPSTREAM 
FLOW INDUCED BY 
JET EXHAUST 
DOWNWASH AT TAIL 
Figure 4.12. Indirect Power Effects. 
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