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keywords:(Wing roots)
Agusta Methodology for Pitch Link Loads Prediction in Preliminary Design Phase
Application of the Root-Locus Method to Aeroelastically Coupled Systems
Comparative Turbulence for a Canberra and a Vulcan Flying Together at Low Altitude
Deflection-Based Aircraft Structural Loads Estimation with Comparison to Flight
Deflection-Based Structural Loads Estimation From the Active Aeroelastic Wing F/A-18 Aircraft
Flow Measurements in the Wake of a Wing Fitted with a Leading-Edge Root Extension (Strake)
Influence of Wing Root Shaping on the Pressure Distribution of Swept-Wing Body Configurations
Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane
Optimization Methods Applied to the Aerodynamic Design of Helicopter Rotor Blades