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Mechanics
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keywords:(Structural Mechanics)
Machine Learning Application on Aircraft Fatigue Stress Predictions
Arecibo Observatory Auxiliary M4N Socket Termination Failure Analysis
Estimation of Effective Elastic Properties of General Carbon/Carbon Honeycomb
Structural Integrity Control Technology Based on Structural Damage Monitoring
Evaluating the Influence of SHM on Damage Tolerant Aircraft Structures Considering Fatigue
Passive Aeroelastic Tailored Wing Modal Test Using the Fixed Base Correction Method
Implementation of Fiber Optic Sensing System on Sandwich Composite Cylinder Buckling Test
Why Should We Encourage Usage of Interference-Fit Fasteners at Airframe Structural Joints?
Conception of Modular Test Stand for Fatigue Testing of Aeronautical Structures
Examination of the KAWAI CLD Method for Fatigue Life Prediction of Composites
Modernizing the A-10 Loading Spectrum Development Process
Bonded Repairs of Composite Panels Representative of Wing Structure
Full-Scale Fatigue Testing from a Structural Analysis Perspective
Study of Composite Impact Dent Visual Detectability and Damage Relaxation Phenomena
Perspective of Structural Health Monitoring for Military Aviation in Poland
Study of Load Spectrum Occurring in the Course of Photogrammetric Missions of the UAV
Flight Testing of an Ultrasonic Based SHM System
A Numerical Approach to the Disbonding Mechanism of Adhesive Joints
Hawk Mk 51/51A/66 Tailplane Full-Scale Fatigue Tests
Comparison of Rivet Hole Expansion for Protruding Rivets; Universal and with Compensator
Bombardier Global 7500 Fatigue Test Cycle Rate Commissioning to ¼ Life
Fatigue of Engineered Metallic Materials Under Constant - and Variable -Amplitude Loading
Approach to Evaluation of Delamination on the MiG-29’s Vertical Stabilizers Composite Skin
Progress on the Pathway to a Virtual Fatigue Test
Strain Controlled Fatigue Testing of Additive Manufactured Titanium Alloy Ti-6Al-4V
Full-Scale Fatigue and Residual Strength Tests of the Composite Wing Box of a Passenger Aircraft
Rapid Calculation of Safe Acceleration Values for Aircraft Structures Under Flight Test
Nondestructive Evaluation for Damage Tolerance Life Management of Composite Structures
Risks of Initial Assumptions in Fatigue and Damage Tolerance of Small Aircraft Development Programs
Weibull or Log-Normal Distribution to Characterize Fatigue Life Scatter – Which Is More Suitable?
Structural Anomaly Detection Using Fiber Optic Sensors and Inverse Finite Element Method
Testing Approach for Over Wing Doors Using Curved Fuselage Panel Testing Technology
Development of Efficient High-Fidelity Solutions for Virtual Fatigue Testing
Simulation of Hypervelocity Impact Effects on Reinforced Carbon-Carbon
Stress-Intensity Factor Solutions for Tapered Lugs with Oblique Pin Loads
A Multiaxial Fatigue Damage Model for Isotropic Materials