Wykaz publikacji wybranego autora

Małgorzata Skorupa, prof. dr hab. inż.

profesor zwyczajny

Wydział Inżynierii Mechanicznej i Robotyki
WIMiR-kwzmk, *Katedra Wytrzymałości, Zmęczenia Materiałów i Konstrukcji


Identyfikatory Autora Informacje o Autorze w systemach zewnętrznych

ORCID: brak

ResearcherID: brak

Scopus: 56419772600

OPI Nauka Polska




1
  • Accounting for the effect of riveting process in fatigue life predictions for lap joints
2
3
  • An experimental investigation of the fatigue performance of riveted lap joints
4
  • An experimental investigation on crack initiation and growth in aircraft fuselage riveted lap joints
5
  • An experimental investigation on crack paths and fatigue behaviour of riveted lap joints in aircraft fuselage
6
  • Analytical, numerical and experimental investigation of the secondary bending of riveted lap joints
7
  • Applicability of empirical formulae for the fatigue notch factor to estimate riveted lap joint fatigue strength
8
  • Applicability of the ASTM compliance offset method to determine crack closure levels for structural steel
9
  • Application of the strip-yield crack closure model to crack growth predictions for structural steel
10
  • Application of the strip-yield model from the NASGRO software to predict fatigue crack growth in aluminium alloys under constant and variable amplitude loading
11
  • Comments to the paper: Fatigue crack growth and life predictions under variable amplitude loading for a cast and wrought aluminum alloy [Glancey CD and Stephens RR. Int J Fatigue, 2006;28:53-60]
12
  • Correlation between experiments and strip yield model results on fatigue crack growth in a structural steel
13
  • Crack growth predictions for structural steel using the strip yield model
14
  • Determination of crack closure for structural steel from local compliance records
15
  • Effect of load transfer by friction on the fatigue behaviour of riveted lap joints
16
  • Effect of production and design related factors on the fatigue behaviour of riveted lap joints in aircraft fuselage
17
18
  • Effect of specimen thickness and stress ratio on fatigue crack growth after a single overload cycle on structural steel
19
  • Evaluation of fatigue crack closure from local compliance measurements in structural steel
20
  • Experimental and theoretical investigation of fatigue crack closure in structural steel
21
  • Experimental tests and prediction of the effect of welding technology on fatigue limit of butt joints in 18G2A steel
22
  • Fatigue crack growth behaviour of 18G2A steel under constant amplitude loading anf following a single overload
23
24
  • Fatigue crack growth in the aluminium alloy D16 under constant and variable amplitude loading
25
  • Fatigue crack location and fatigue life for riveted lap joints in aircraft fuselage