Mehrdad Pourjam
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Mehrdad Pourjam has a total of 13 co-authors. Here are the top co-authors by number of shared publications:
- Kavan Hazeli
Aerospace and Mechanical Engineering Department The University of Arizona Tucson Arizona USA
5 shared publications - Gabriel Demeneghi
NASA Marshall Space Flight Center, 4602 Martin Rd SW, Huntsville, AL 35808, USA
3 shared publications - Paul R. Gradl
NASA Marshall Space Flight Center, Huntsville, USA
3 shared publications Daniel June
2 shared publicationsTimothy M. Smith
2 shared publications- Brandon J. Colón
Department of Aerospace and Mechanical Engineering, The University of Texas at El Paso, El Paso, TX 79968, USA
1 shared publication
Latest Publications
- Open Access
- 27 May 2026
- Published by Elsevier in Journal of Materials Research and Technology
- Vol. 42, 10639-10655
Yield surface characterization of GRX-810: Linking texture, microstructure, and anisotropic behavior
- 27 May 2026
- Published by Elsevier in Journal of Materials Research and Technology
- Vol. 42, 10639-10655
Open AccessYield surface characterization of GRX-810: Linking texture, microstructure, and anisotropic behavior
- 17 October 2025
- Published by Elsevier in Materials Science and Engineering: A
- Vol. 948
GRX-810: High-temperature behavior, deformation mechanisms, and size effects
- 17 October 2025
- Published by Elsevier in Materials Science and Engineering: A
- Vol. 948
GRX-810: High-temperature behavior, deformation mechanisms, and size effects
- 14 December 2024
- Published by Elsevier in Additive Manufacturing
- Vol. 97
High-temperature behavior of additively manufactured Haynes 214: Ductility loss and deformation mechanisms transition
- 14 December 2024
- Published by Elsevier in Additive Manufacturing
- Vol. 97
High-temperature behavior of additively manufactured Haynes 214: Ductility loss and deformation mechanisms transition
- Open Access
On the Mechanical Behavior of LP-DED C103 Thin-Wall Structures
Laser Powder Directed Energy Deposition (LP-DED) can produce thin-wall features on the order of 1 mm. These features are essential for large structures operating in extreme environments such as regeneratively cooled nozzles and heat exchangers, which often make use of refractory metals. In this work, the mechanical behavior of LP-DED C103 was investigated via quasi-static tensile testing and low cycle fatigue (LCF) testing. The effects of vacuum stress relief (SR) and hot isostatic pressing (HIP) heat treatments were investigated for specimens in the vertical and horizontal build orientations during tensile testing. The AB and SR properties were lower than literature values for wrought and laser powder bed fusion (L-PBF) bulk components but higher than electron beam powder bed fusion (EB-PBF). The application of a HIP cycle improved strength by 7% and ductility by 27% past the initial as-built condition. Fracture images reveal that interlayer stress concentration sites are responsible for fracture in specimens in the vertical orientation. Meanwhile, fracture in the horizontal specimens mainly propagates at a slanted angle typical of plane stress conditions. The LCF results show cycles to failure ranging from 100 cycles to 8000 cycles for max strain levels of 2% and 0.5%, respectively. Fractography on the fatigue specimens reveals an increasing propagation zone as max strain levels are increased. The impact of these findings and future work are discussed in detail.
Open AccessOn the Mechanical Behavior of LP-DED C103 Thin-Wall Structures
Laser Powder Directed Energy Deposition (LP-DED) can produce thin-wall features on the order of 1 mm. These features are essential for large structures operating in extreme environments such as regeneratively cooled nozzles and heat exchangers, which often make use of refractory metals. In this work, the mechanical behavior of LP-DED C103 was investigated via quasi-static tensile testing and low cycle fatigue (LCF) testing. The effects of vacuum stress relief (SR) and hot isostatic pressing (HIP) heat treatments were investigated for specimens in the vertical and horizontal build orientations during tensile testing. The AB and SR properties were lower than literature values for wrought and laser powder bed fusion (L-PBF) bulk components but higher than electron beam powder bed fusion (EB-PBF). The application of a HIP cycle improved strength by 7% and ductility by 27% past the initial as-built condition. Fracture images reveal that interlayer stress concentration sites are responsible for fracture in specimens in the vertical orientation. Meanwhile, fracture in the horizontal specimens mainly propagates at a slanted angle typical of plane stress conditions. The LCF results show cycles to failure ranging from 100 cycles to 8000 cycles for max strain levels of 2% and 0.5%, respectively. Fractography on the fatigue specimens reveals an increasing propagation zone as max strain levels are increased. The impact of these findings and future work are discussed in detail.