Wireless Energy Supply to Aircraft Structural Health Monitoring Nodes Using Ultrasonic Lamb Waves
Verification of the Computed Tomography Results of Aluminum Alloy Welded Joint
The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe
The Role Of Leadership In Aviation Safety And Aircraft Airworthiness
The In-Depth Stress Distribution for 1H13 Specimen after Cutting
The Impact of Damage in Inconel 718 on Hardness Measured by the Vickers Method
The Impact of Damage in Anneling Inconel 718 on Hardness Measured by the Vickers Method
The Fractographic Investigation of an Aeroengine Accessory Gearbox Quill Shaft
The Fatigue Life of Cables in Aircraft Flight Control Systems
The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System
The Effect of Superalloy Structure on Ultrasonic Wave Parameters
The Effect of Environmental Flight Conditions on Damage Propagation in Composite Sandwich Structure
The Effect of Anodizing Process Parameters on the Fatigue Life of 2024-T-351-Aluminium Alloy
The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test
The Concept of a Full Scale Fatigue Test of a Su-22 Fighter Bomber
The Application of Acoustic Anisotropy to Evaluation of Material Properties
Synchrotron Radiation Application for Lattice Strain Measurements
Stress Analysis of the PZL M28’s Airframe Subjected to Repairs During Fatigue Tests
Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems
Simulating Crack Propagation of a Selected Structural Component of the PZL-130 Orlik TC-II Aircrafts
Selected Aspects Related to the Applied Loads Control During Fatigue Tests of a Metallic Airframe
Selected Aspects Related to Preparation of Fatigue Tests of a Metallic Airframe
Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe
Review of Aeronautical Fatigue Investigations in Poland (2013-2014)
Research on Hovercraft – Fatigue Cracks in the Engine Frame
Preparation of Samples used in Fatigue Testing of Aircraft Materials
Prediction of Fatigue Cracks Using Gamma Function
Possibile Applications of Magnetic Microwires in Aviation
Nonlinear Fatigue Damage Accumulation
Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions
Micromechanical Properties and Stress Measurements with Diffraction Methods
Mi-24 Helicopter Full Scale Fatigue Test Concept
Methods for Different Orders Stresses Estimation with Diffraction Methods
Mechanical Tests Applied to Structural Health Monitoring: An Overview of Previous Experience
Low-Cost Data Acquisition Unit for Flight Tests
Local Phenomena During Riveting Process
Load Spectrum Analysis with Open Source Software – An Application Example
Lightning Strike Protection of Aircraft Composite Structures: Analysis and Comparative Study
Lift Force Measurement in Landing Gears Dynamic Tests
Investigations into Load Spectra of UAVS Aircraft