Maria Jesus Perez-Martin

Dr. Maria Jesus Perez-Martin

Mondragon University, Faculty of engineering
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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1 July 2014 in International Journal of Impact Engineering
Verified
Journal Article
Open access
BEBorja Erice
Borja Erice
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
FGFrancisco Gálvez
Francisco Gálvez
A numerical and experimental study of ballistic impacts at various temperatures on precipitation hardened Inconel 718 nickel-base superalloy plates has been performed. A coupled elastoplastic-damage constitutive model with Lode angle dependent failure criterion has been implemented in LS-DYNA non-linear finite element code to model the mechanical behaviour of such an alloy. The ballistic impact tests have been carried out at three temperatures: room temperature (25 °C), 400 °C and 700 °C. The numerical study showed that the mesh size is crucial to predict correctly the shear bands detected in the tested plates. Moreover, the mesh size convergence has been achieved for element sizes on the same order that the shear bands. The residual velocity as well as the ballistic limit prediction has been considered excellent for high temperature ballistic tests. Nevertheless, the model has been less accurate for the numerical simulations performed at room temperature, being though in reasonable agreement with the experimental data. Additionally, the influence that the Lode angle had on quasi-static failure patterns such as cup-cone and slanted failure has been studied numerically. The study has revealed that the combined action of weakened constitutive equations and Lode angle dependent failure criterion has been necessary to predict the previously-mentioned failure pattern

19 April 2013 in Journal of Applied Mechanics
Verified
Journal Article
Closed access
PDF file
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
Alejandro EnfedaqueAlejandro Enfedaque
Alejandro Enfedaque
WDW. Dickson
W. Dickson
FGF. Gálvez
F. Gálvez

1 December 2013 in Scripta Materialia
Verified
Journal Article
Open access
AJAntoine Jérusalem
Antoine Jérusalem
WDWilliam Dickson
William Dickson
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
Ming DaoMing Dao
Ming Dao
JLJian Lu
Jian Lu
FGFrancisco Gálvez
Francisco Gálvez

7 September 2018 in EPJ Web of Conferences
Verified
Journal Article
Open access
APAntonio Pellegrino
Antonio Pellegrino
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
KDKalin Dragnevski
Kalin Dragnevski
GZGiuseppe Zumpano
Giuseppe Zumpano
NPNik Petrinic
Nik Petrinic
Abradable coatings are utilised as sacrificial materials in low-pressure compressor casings, and in intermediate and high pressure compressors and seals. The adoption of abradable coatings allows for the clearance between compressor blades and casing to be minimised, increasing the overall efficiency of the engine. Quasi-static and dynamic experiments at different temperatures are conducted to characterise the mechanical response of a thermally-sprayed abradable seal coating. The material is composed of an aluminium continuum matrix and fairly well-dispersed polyester particles. Stress versus strain histories are measured in uniaxial tension and compression at strain rates ranging from 10-3 to 102 s-1, via non-standard experimental techniques. The material displays sensitivity to the strain rate and to the imposed temperature. The mechanical behaviour is brittle in tension while it exhibits higher strains to failure in compression. The material is characterised by a pronounced tension/compression asymmetry.

1 January 2019 in Engineering Fracture Mechanics
Verified
Journal Article
Closed access
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
BEBorja Erice
Borja Erice
FGFrancisco Galvez
Francisco Galvez

24 June 2019 in Journal of Dynamic Behavior of Materials
Verified
Journal Article
Open access
PDF file
MPMaria Jesus Perez-Martin
Maria Jesus Perez-Martin
JHJ. K. Holmen
J. K. Holmen
STS. Thomesen
S. Thomesen
OHO. S. Hopperstad
O. S. Hopperstad
TBT. Børvik
T. Børvik
The main objective of this experimental study is to determine the effect of low temperatures on the mechanical behaviour of Strenx 960 Plus high-strength structural steel at different strain rates and stress triaxialities. For this purpose, a comprehensive experimental campaign was designed to characterise the material at a wide range of temperatures and loading rates. The stress triaxiality was varied by testing specimens with different geometry. First, to determine the ductile-to-brittle transition temperature, instrumented Charpy V-notch impact tests were carried out at a range of temperatures from + 20 °C down to − 90 °C. The impact energy dropped gradually with decreasing temperature, but a clear transition temperature could not be identified. A fractography study exhibited a clear dimple structure, revealing predominantly ductile fracture at all temperatures. Then, uniaxial tension tests on smooth and pre-notched axisymmetric specimens under both quasi-static and dynamic loading rates were carried out at room temperature and low temperatures. These tests were conducted to characterise the rate-dependence of the stress–strain behaviour and the failure strain. The results revealed that under quasi-static conditions the flow stress increased with decreasing temperature, while the failure strain was nearly independent of the temperature. Dynamic tensile tests using the same specimen geometries were conducted in a split Hopkinson tension bar at + 20 °C and − 40 °C. The material exhibited a positive strain rate sensitivity at all investigated temperatures. This experimental study reveals that the Strenx 960 Plus steel retains its ductility at temperatures as low as − 40 °C. Brittle failure could not be observed even with combined high strain rate, high stress triaxiality and low temperature.