1965 datcom sections6 9

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  • 6.1.1 - Control Devices - Section Lift6.1.2 - Contol Devices - Section Pitching Moment6.1.3 - Control Devices - Section Hinge Moment6.1.4 - Control Devices - Lift6.1.5 - Control Devices - Pitching Moment6.1.6 - Control Devices - Hinge Moment6.1.7 - Control Devices - Drag6.2.1 - Control Devices - Rolling Moment6.2.2 - Control Devices - Yawing Moment7 - Dynamic Derivatives7.1.1 - Wing Pitching Derivatives7.1.2 - Wing Rolling Derivatives7.1.3 - Wing Yawing Derivatives7.1.4 - Wing Acceleration Derivatives7.2.1 - Body Pitching Derivatives7.2.2 - Body Acceleration Derivatives7.3.1 - Wing-Body Pitching Derivatives7.3.2 - Wing-Body Rolling Derivatives7.3.4 - Wing-Body Acceleration Derivatives7.4.1 - Wing-Body-Tail Pitching Derivatives7.4.4 - Wing-Body-Tail Acceleration Derivatives8.1 - Mass and Inertia - Aircraft8.1 - Mass and Inertia - Missiles9 - VTOL-STOL Aircraft9.1 - Free Propeller Characteristics9.1.1 - Propeller Thrust9.1.2 - Propeller Pitching Moment9.1.3 - Propeller Normal Force9.2 - Propeller-Wing Characteristics9.2.1 - Propeller-Wing Lift9.2.3 - Propeller-Wing Drag9.3 - Ducted Propeller Characteristics9.3.1 - Ducted Propeller Lift9.3.2 - Ducted Propeller Pitching Moment9.3.3 - Ducted Propeller Drag