Program



 

CONFERENCE PROGRAMME

15 JANUARY 2009

10:00

Registration and welcome speech

Antoni Niepokólczycki

10:30

FAR-23 Commuter Category Airplane Fatigue Tests in PZL Mielec

Janusz Pietruszka

11:15

-          Romanian Aeronautical Industry

-          The Rivet Parameter Influence in Fatigue Strength

-          Numerical Models for Fatigue Crack Evolution Study

Ion Fuiorea

12:00

Break

 

12:30

The Mi-2 Helicopter’s Blade Material Testing

Marcin Kurdelski

13:00

The fatigue Life Assessment of PZL-130 ORLIK Structure Based on Historical Usage Data

Andrzej Leski

13: 30

In-service Flaw Detection and Quantification in the Composite Structures of the Aircraft

Piotr Synaszko

14:00

Break

 

14:45

Application of Array Form of Load Spectra in Fatigue Evaluation of Aeronautical Composite Structures

Mirosław Rodzewicz

15:15

Load Spectrum of a Glider Chassis

Wojciech Owczarek

15:45

The Application of FEM to Determine the Loads Applied during the Acoustic Fatigue Tests of Aircraft Structures

Andrzej Szot

16:15

End

 

19:00

Conference dinner

 

16 JANUARY 2009

10:00

OLYMPUS Presentation

 

11:00

Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading

Petr Augustin

11:30

Strenght Calculations and Investigations of the Air-landing Troops Rope Console for Helicopter Type Mi-17”

Andrzej Szot

12:00

Break

 

12:30

Fatigue Damage of Rivet Joints in the Condition of Stable Cyclic Load

Volodymyr Hutsaylyuk

13:00

Methods for FEM Analysis of Riveted Joints of Thin-Walled Aircraft Structures within IMPERJA Project

Wojciech Wronicz

13:30

End