C-130 Hercules
  E-2C Hawkeye
  Wind Tunnel testing
  e-2c wind tunnel tests
  specific e-2c problems
  directional stability
  > roll control
  pitch stability
  stall speeds
  max lift coefficient comparison
  CLmax vs flap
deflection
  flaps 10 deficiencies
  tunnel
characteristics
  wing fatique life
  vibration
  blr test approach
  thrust coefficient vs airspeed
Roll Control
High adverse yaw caused by the following:
• Poor Directional Stability
•
Unusual aileron deflections at landing flaps
aggravates adverse yaw.

 

 
 



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