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BIEGEBEANSPRUCHUNG
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About the Strength of a Rail with an Internal Transverse Crack
Abrams and Heavy Equipment Transporter Bridge Crossing Capability Analysis
A bumper model with dynamic contact stiffness for simulations of pedestrian legform impacts
Acht Millimeter. Mechanische Festigkeit mit modernen Kondensatortechnologien verbessern
A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics. Part III. Program Manual
A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics. Part II. User's Manual
Acoustic Scattering by Laminated Plates with Viscoelastic Layers
Action Path and Mechanism of Segment Joints in the Failure History of Shield Tunnel Lining
Active aeroelastic control over a multisurface wing: modeling and wind-tunnel testing
Active control of inverted cantilever-beam: Preliminary study for deck-house vibration control
Active radial system of railway vehicles based on secondary suspension rotation angle sensing
Active Suppression of Aeroelastic Instabilities for Forward Swept Wings
Active Vibration Control of Flexible Rotors on Maneuvering Vehicles
Adaptive finite element technique for thermal stress analysis of built-up structures
Adaptive notch filter design for bending vibration of a sounding rocket
Adaptive Underactuated Finger with Active Rolling Surface
Advanced control systems for the Saturn V launch vehicle.
Advanced Dual-Pull Mechanism for Deployable Spacecraft Booms
Advanced optical rotor blade deformation measurements on a flying helicopter
Aerodynamic Design Optimization Using the Drag-Decomposition Method
Aerodynamic Optimization Trade Study of a Box-Wing Aircraft Configuration
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods
Aerodynamic Shape Optimization of an Adaptive Morphing Trailing-Edge Wing
Aeroelastic Bending Analysis of a Terrier-Tomahawk 9 Sounding Rocket Vehicle
Aeroelastic Divergence of Unguided Missiles by Dynamics Analysis
Aeroelasticity of Axially Loaded Aerodynamic Structures for Truss-Braced Wing Aircraft
Aeroelastic Optimization of Aircraft Wings Using a Coupled Three-Dimensional Panel-Beam Model
Aeroelastic sensitivity analysis of wings using automatic differentiation
Aeroelastic Stability of a Four-Bladed Semi-Articulated Soft-Inplane Tiltrotor Model