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deformation
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keywords:(Wing deformation)
Shape optimisation of blended-wing-body underwater gliders based on free-form deformation
Design, kinematic and fluid-structure interaction analysis of a morphing wing
A new jig-shape optimization method for the high aspect ratio wing
Aeroelastic Demonstrator Wing Design for Maneuver Load Alleviation Under Cruise Shape Constraint
Dynamic Damage of Aircraft Wing Leading Edge Impacted by Birds
Experimental Aeroelastic Benchmark of a Very Flexible Wing
In Situ Imaging of Parachute Textile Micromechanics Under Tensile Load
Optimization of spar mass and fuselage location to decrease loss of airplane lift force
Flutter Predictions for Very Flexible Wing Wind Tunnel Test
Dynamic behavior of wing leading edge assembly with thermal protection coating
Dynamic behavior of wing leading edge assembly with thermal protection coating
Modal Rotations: A Modal-Based Method for Large Structural Deformations of Slender Bodies
Accurate Stick Model Development for Static Analysis of Complex Aircraft Wing-Box Structures
Multidimensional Models for Double-Swept Helicopter Blades
Dynamic Distributed Morphing Control of an Aeroelastic Wing for a Small Drone
Geometrically Nonlinear Structural Modal Analysis Using Fictitious Masses
Nonlinear Static Aeroelastic and Trim Analysis of Highly Flexible Joined-Wing Aircraft
Buckling Optimization of Variable-Angle-Tow Panels Using the Infinite-Strip Method
Aeroelastic Deformation Measurements of Flap, Gap, and Overhang on a Semispan Model
Aeroelastic Analysis of Wing Structures Using Equivalent Plate Models
Static Load Tests on an Lfu 205 Wing of Spanwise Tubular Construction
Structural Design of Man Powered Aircraft
The "fish-mouth" actuator: design issues and test results
Overview of the Transport Rotorcraft Airframe Crash Testbed (TRACT) Full Scale Crash Tests
Optical Measurement, of Missile Wing Deformation in High Velocity Tests
Modelling and analysis of coupled flap-lag-torsion vibration characteristics helicopter rotor blades
Determination of Stores Pointing Error Due to Wing Flexibility under Flight Load
Deflection-Based Aircraft Structural Loads Estimation with Comparison to Flight
Effects of Aeroelastic Deformation on the Unaugmented Stopped-Rotor Dynamics of an X-Wing Aircraft
Aeroelastic Effects of Transverse Shear Deformation on Composite Wings in Various Speed Flow Regimes
Static Aeroelastic Analysis of a Three-Dimensional Generic Wing
Influence of Structural Flexibility on Flapping Wing Propulsion
Evaluation of the First Transport Rotorcraft Airframe Crash Testbed (TRACT 1) Full-Scale Crash Test
F-111 Stiffener Run Out Number 2 Parametric Study