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abrupt absolute coefficient Aeronautical aileron deflection aileron rolls aileron servo airspeed amplitude apparatus APPLICATION approach condition approximately axis caused changes characteristics circuit Cleveland computed considered conventional cruising condition damping desired determine dihedral effect direction drive dynamic effective dihedral error evaluation Field flight force forward function gearing given histories increased indicated initial intolerable knots Laboratory landing landing-approach condition lateral oscillations limit maximum measured motion negative normal airplane obtained operation opinions period pilots plane positive possible present range ratio references requirements reversals rolling response rolling velocity rotation rudder rudder kicks seen servo motor servo-gearing ratio servomechanism showed shown in figure sideslip angle signal simulate speed static stick stick-fixed stick-free test airplane tion tolerable tolerable effective dihedral torque tube trim typical United values vane variation varies wing yawing zero
Page 16 - Pearson, Henry A., and Jones, Robert T., "Theoretical Stability and Control Characteristics of Wings with Various Amounts of Taper and Twist,
Page 16 - Liddell, Charles J., Jr.; Van Dyke, Rudolph D., Jr.; and Heinle, Donovan R.: A Flight Determination of the Tolerable Range of Effective Dihedral on a Conventional Fighter Airplane.