Photo of Daniel Leidermark

Daniel Leidermark

Senior Associate Professor

Mainly, my research is focused on the behaviour of single-crystal nickel-base superalloys. Investigation is centered around the mechanical behaviour, through experimental observation and modelling of these. I teach within solid mechanic courses.

High temperature mechanics – a constitutive behaviour approach to fatigue issues

The trend in the global electricity generation is changing towards a state where green energy, e.g. hydro, wind or solar power, will become the largest power source. With this increasing supply from green energy the need to be able to balance the power output is fundamental. A way to accomplish this is to use gas turbines as the bridge to green energy. 

These can be taken online or offline in a matter of minutes to produce power, a suitable balancer to the green energy sources. The rapid changes in energy production set high reliability on the gas turbines components. These changes introduce a cyclic exposure of the components which leads to thermomechanical fatigue load conditions. 

At peak loading the components will be subjected to high temperature in combination with high mechanical load, hence exposed to creep/stress relaxation. 

The increased usage of gas turbines on the energy market sets high demands on the environmental impact and efficiency, meaning that better prediction methods and more realistic behaviour of the materials are needed in the simulations during the design phase. 

Single-crystal nickel-base superalloys

The major class of materials used for the first stage turbine blades is single-crystal nickel-base superalloys, due to their excellent high temperature properties. See Fig. 1 for a typical microstructure image of a single-crystal superalloy. These blades are manufactured through investment casting, a perfectly aligned specimen is never achieved during this process, hence misalignments in crystal orientation need to be accounted for, see Fig. 2. 

However, the anomalous elastic and inelastic material behaviour of single-crystal nickel-base superalloys makes the evaluation/design process rather complex, see Fig. 3. Hence, insufficient knowledge of the material behaviour often leads to the use of large safety factors that leads to conservative designs, which in turn render loss in performance and efficiency.



Thomas Lindström, Daniel Nilsson, Kjell Simonsson, Robert Eriksson, Jan-Erik Lundgren, Daniel Leidermark (2024) Constitutive model of an additively manufactured combustor material at high-temperature load conditions Materials at High Temperature Continue to DOI
Daniel Leidermark, Magnus Andersson (Editorship) (2024) Reports in Applied Mechanics 2022


Ahmed Azeez, Daniel Leidermark, Robert Eriksson (2023) Stress intensity factor solution for single-edge cracked tension specimen considering grips bending effects Procedia Structural Integrity, Vol. 47, p. 195-204 Continue to DOI
Håkan Andersson, Joakim Holmberg, Kjell Simonsson, Daniel Hilding, Mikael Schill, Daniel Leidermark (2023) Simulation of wear in hydraulic percussion units using a co-simulation approach International Journal of Modelling and Simulation, Vol. 43, p. 265-281 Continue to DOI
Stefan B. Lindstrom, Johan Moverare, Jinghao Xu, Daniel Leidermark, Robert Eriksson, Hans Ansell, Zlatan Kapidzic (2023) Service-life assessment of aircraft integral structures based on incremental fatigue damage modeling International Journal of Fatigue, Vol. 172, Article 107600 Continue to DOI

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  • PhD Solid Mechanics, Linköping University, Sweden 2011
  • Lic. Solid Mechanics, Linköping University, Sweden 2010
  • MSc Mechanical Engineering, Linköping University, Sweden 2008
  • BSc Mechanical Engineering, Växjö University, Sweden 2004


You can find publications related to Daniel Leidermarks work at Scopus.

Research interest

  • High temperature mechanics
  • Constitutive modelling
  • Single-crystal superalloys
  • Crack initiation and propagation
  • Thermomechanical fatigue


  • Solid Mechanics, basic course (TMMI17)
  • Advanced material and computational mechanics (TMHL19)