Fatigue of Aircraft Structures

Titel Veröffentlichungsdatum Sprache Zitate
Experimental and Numerical Study of Strain Progress During and After Riveting Process for Brazier Rivet and Rivet with Compensator - Squeezing Force and Rivet Type Effect2011/01/016
In-Service Flaw Detection and Quantification in the Composite Structures of Aircraft2009/07/266
Flight Loads Acquisition for PZL-130 Orlik TCII Full Scale Fatigue Test2011/01/015
Stress Intensity Factor Calculations for the Compressor Blade with Half-Elliptical Surface Crack Using Raju-Newman Solution2011/08/015
Damage Detection and Size Quantification of FML with the Use of NDE2012/01/013
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin2009/07/263
Experimental and Numerical Crack Initiation Analysis of the Compressor Blades Working in Resonance Conditions2011/08/013
Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading2010/12/013
The Synthetic Description of the Results, Scientific Achievements and Practical Applications of the Eureka − Imperja Project, E3496! − “Improving the Fatigue Performance of Riveted Joints in Airframes”2012/12/013
Numerical Simulation of Fatigue Fracture of the Turbine Disc2012/01/012
An Approach to Damage Detection in the Aircraft Structure with the Use of Integrated Sensors – The Symost Project2012/12/012
Using Sandblasting and Sol Gel Techniques for the Preparation of a Metal Surface and Their Effects on the Durability of Epoxy-Bonded Joints2012/12/012
Numerical Models for Fatigue Crack Evolution Study2009/07/262
Experimental Crack Propagation Analysis of the Compressor Blades Working in High Cycle Fatigue Condition2009/01/262
Investigation into Fatigue Behaviour of Metal-Composite Glue Connection2011/08/012
Compressor Blade Fatigue Diagnostics and Modelling with the Use of Modal Analysis2011/01/012
Monitoring of Crack Growth in a Structure Under a Composite Patch2011/01/012
Stress Intensity Factor Analysis and Fatigue Behavior of A Crack in The Residual Stress Field of Welding2011/01/012
The Rivet Parameter Influence in Fatigue Strength2009/01/261
Investigations Into Glider Chassis Load Spectrum2009/01/261
Introduction of Fatigue Markers in Full Scale Fatigue Test of an Aircraft Structure2012/12/011
Full Scale Fatigue Test of New Undercarriage for Commuter Aircraft2012/01/011
Methods for Global and Local FEM Analysis of Riveted Joint on the Example of the PZL M28 Skytruck Aircraft2009/01/261
Deterministic Approach to Predicting the Fatigue Crack Growth in the 2024-T3 Aluminum Alloy Under Variable Amplitude Loading2009/07/261
Analysing Micromechanisms of Initiation and Propagation of Short Fatigue Cracks from Rivet Holes in the Aluminums Sheets2009/07/261
Analysis of the Possibility to Assess the Occurrence of Hidden Corrosion in Lap Joints Using Active Thermography2011/01/011
The Effect of Electrochemical Machining on the Fatigue Strength of Heat Resistance Alloys2011/01/011
Service Life Assessment Program of PZL-130 Orlik TCII Structure2011/08/011
Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft2011/01/011
Investigations of Some Properties of Material Samples Taken from the Aircraft Withdrawn from Service2010/01/011