Contents: Aerodynamic Mathematical Modeling - Basic Concepts; Impact of High-Alpha Aerodynamics on Dynamic Stability Parameters of Aircraft and Missiles; Review of Techniques for Determination of Dynamic Stability Parameters in Wind Tunnels; Direct Forced-Oscillation Techniques for the Determination of Stability Derivatives in Wind-Tunnels; Wind Tunnel Measurement of Aerodynamic Derivatives Using Flexible-Sting Rigs; Rotary and Magnus Balances; Curved-Flow, Rolling Flow and Oscillatory PUre-Yawing Wind-Tunnel Test Methods for Determination of Dynamic Stability Derivatives; Support Interference; Applications of Half-Model Technique in Dynamic Stability Testing; Determination of Aircraft Dynamic Stability and Control Parameters from Flight Testing; Estimation of Dynamic Stability Parameters from Drop Model Flight Tests; Analytical Determination of Dynamic Stability Parameters; Aeroelasticity, Including Dynamic Effects of Separated Flow; Control Derivatives; Sensitivity of Aircraft Motion to Cross-Coupling and Acceleration Derivatives; Some Applications of Aerodynamic Formulations to Problems in Aircraft Dynamics; Applications of Dynamic Stability Parameters to Problems in Aircraft Dynamics; and Application to Missile Dynamics.
Dynamic Stability Parameters
1981
391 pages
Report
No indication
English
Aerodynamics , Aircraft , Missile Technology , Aerodynamic stability , Guided missiles , Dynamic response , Mathematical models , Stability , Angle of attack , Roll , Oscillation , Yaw , Pitch(Motion) , Aeroelasticity , Flow separation , Coupling(Interaction) , Acceleration , Aerodynamic characteristics , Flight maneuvers , Wind tunnel tests , Flight testing , Dynamic tests , Sting mounts , Flexible structures , Lectures , Foreign technology , Dynamic stability , NATO furnished , High angles
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