Ismet Baran

Dr. Ismet Baran

University of Twente, The Netherlands
orcid

Research Focus & Metrics

Academic Career Length

15Years (2012-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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20 January 2016 in Archives of Computational Methods in Engineering
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Journal Article
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Ismet BaranIsmet Baran
Ismet Baran
KCKenan Cinar
Kenan Cinar
NENuri Ersoy
Nuri Ersoy
RARemko Akkerman
Remko Akkerman
JHJesper Hattel
Jesper Hattel
The increased usage of fiber reinforced polymer composites in load bearing applications requires a detailed understanding of the process induced residual stresses and their effect on the shape distortions. This is utmost necessary in order to have more reliable composite manufacturing since the residual stresses alter the internal stress level of the composite part during the service life and the residual shape distortions may lead to not meeting the desired geometrical tolerances. The occurrence of residual stresses during the manufacturing process inherently contains diverse interactions between the involved physical phenomena mainly related to material flow, heat transfer and polymerization or crystallization. Development of numerical process models is required for virtual design and optimization of the composite manufacturing process which avoids the expensive trial-and-error based approaches. The process models as well as applications focusing on the prediction of residual stresses and shape distortions taking place in composite manufacturing are discussed in this study. The applications on both thermoset and thermoplastic based composites are reviewed in detail.

1 August 2013 in Composites Part B: Engineering
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Journal Article
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Ismet BaranIsmet Baran
Ismet Baran
CTCem C. Tutum
Cem C. Tutum
MNMichael W. Nielsen
Michael W. Nielsen
JHJesper Hattel
Jesper Hattel

28 February 2017 in Advances in Materials Science and Engineering
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EHEva C. Hofland
Eva C. Hofland
Ismet BaranIsmet Baran
Ismet Baran
DWDagmar A. Wismeijer
Dagmar A. Wismeijer
Selective laser sintering (SLS) is an additive manufacturing technique that enables the production of customized, complex products. SLS has proven itself a viable prototyping tool and production method for noncritical products. The industry has picked up on the potential of SLS, which raised the question whether it is possible to produce functional products with reproducible mechanical properties for application in critical sectors. Properties of SLS parts highly depend on the applied process settings. Hence, present work examined the influence of key process parameters (preheating temperature, laser power, scan spacing, scan speed, layer thickness, and part build orientation) on the properties (tensile strength, tensile modulus, elongation at break, and part density) of SLS produced parts. A design of experiments (DoE) approach was used to plan the experiments. Test samples according to DIN EN ISO 527-2 were produced on a sintering system (EOSINT P395) using polyamide 12 powder (EOS PA2200). Regression models that describe the relation between the process settings and resulting part properties were developed. Sensitivity analysis showed that mechanical properties of sintered parts were highly affected by layer thickness and scan spacing variations.

1 January 2013 in Energy Procedia
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Journal Article
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UPUwe Schmidt Paulsen
Uwe Schmidt Paulsen
HMHelge Aagård Madsen
Helge Aagård Madsen
JHJesper Hattel
Jesper Hattel
Ismet BaranIsmet Baran
Ismet Baran
PNPer Hørlyck Nielsen
Per Hørlyck Nielsen
This paper outlines results of a proposed layout of a light 2-bladed rotor, with a driving torque constraint matching the generator design, and shows details of the pultruded blade – and rotor geometry. In comparison with the 1st baseline design of a 5 MW VAWT concept this present development provides during standstill and operation significant less mass with a comparable level of loading strain in the blades and in the junctions between blade and tower. Optimized blade profile having a low weight and high stiffness is obtained according to the design evaluations based on the standstill calculations in ANSYS software. The selected profiles are used in the aero dynamic simulation. Furthermore the simulation code will be demonstrated to show the fully development model, integrating the simulation of turbulent wind inflow, actuator cylinder flow model, power controls, hydraulic floater - and mooring line systems implementation

1 August 2014 in Composites Part B: Engineering
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Journal Article
Closed access
Ismet BaranIsmet Baran
Ismet Baran
RARemko Akkerman
Remko Akkerman
JHJesper Hattel
Jesper Hattel

1 December 2020 in Composites Part B: Engineering
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Journal Article
Closed access
NHNing Han
Ning Han
Ismet BaranIsmet Baran
Ismet Baran
JZJamal Seyyed Monfared Zanjani
Jamal Seyyed Monfared Zanjani
OYOnur Yuksel
Onur Yuksel
LALuLing An
LuLing An
RARemko Akkerman
Remko Akkerman