MAVWEPS 00-BOT-80 
APPLICATION OF AEBODYNAMICS 
TO SPECIFIC PBOBLEMS OF FLYING 
ROTOR BLADE ELEMENT 
RELATIVE - 
ROTATION WIND COMPONENT 
DUE TO ROTATION 
LOCAL FLOW AT BLADE ELEMENT 
VELOCITY DUE 
RESULTANT 
RELATIVE VELOCITY 
--_ 
TIP PATH PLANE 
Figure 6.75. Rotor Blade Flemenf Aerodynamics 
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