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Review of Aeronautical Fatigue Investigations in Poland (2013-2014)
Fatigue Degradation of the Structure of Parachute Systems
The Role Of Leadership In Aviation Safety And Aircraft Airworthiness
Low-Cost Data Acquisition Unit for Flight Tests
Impact of Carbon Nanotubes on the Mechanical and Electrical Properties of Silicone
Evaluation of Damage Degree of Inconel 718 using Nondestructive Indicators of Damage
Load Spectrum Analysis with Open Source Software – An Application Example
Lightning Strike Protection of Aircraft Composite Structures: Analysis and Comparative Study
Dynamic Fatigue Tests Of Landing Gears
Experimental Validation of Riveting Process Fe Simulation
Aircraft Corrosion – Review of Corrosion Processes and its Effects in Selected Cases
Electropolishing Procedure Dedicated to In-Depth Stress Measurements with X-Ray Diffractometry
Automatic traceabillty from tests to requirements by requirement-based refinement
The Effect of Anodizing Process Parameters on the Fatigue Life of 2024-T-351-Aluminium Alloy
Study of fretting fatigue crack initiation for riveted Al 6xxx components
Research on Hovercraft – Fatigue Cracks in the Engine Frame
Mechanical Tests Applied to Structural Health Monitoring: An Overview of Previous Experience
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
Experimental and Numerical Study of NACA and Conventional Riveting Procedure
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe
Impact Loads and Crash Safety of the Cockpit of a Composite Glider
Mi-24 Helicopter Full Scale Fatigue Test Concept
Eddy current flexible probes for complex geometries
The Fatigue Life of Cables in Aircraft Flight Control Systems
FEATURES OF FORMATION OF FUNCTIONAL COVERINGS AT ELECTROSPARK MODIFYING OF METAL MATERIALS
Investigations into Load Spectra of UAVS Aircraft
Advanced Magnetic Materials for Aeronautics
The Impact of Damage in Inconel 718 on Hardness Measured by the Vickers Method
Automation of Aircraft Fatigue Life Estimation
The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure
The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System
Stress Analysis of the PZL M28’s Airframe Subjected to Repairs During Fatigue Tests