Applied sciences

Archives of Metallurgy and Materials

Content

Archives of Metallurgy and Materials | 2026 | vol. 71 | No 1

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Abstract

Material extrusion additive manufacuring (MEAM) is a universally adopted additive manufacturing (AM) process for fabricating custom-designed fiber-reinforced thermoplastic composite items; providing affordability, rapid production, and reduced material waste. However, the significant limitations are weaker mechanical performance and surface smoothness. This paper focuses on the optimization of different post-processing and thermal conditions to enhance tensile performance, hardness (shore D), and surface texture of carbon fiber-reinforced polylactic acid (CFPLA) objects. The novelty of this investigation is to systematically examine the effect of separate and combined post-processing treatment, applied in various cooling conditions and sequences, to evaluate their respective influence on overall performance including mechanical and surface attributes. The result demonstrates that different post-processing condition showed different effect on output responses, tensile strength, durometer hardness (Shore D), and roughness profile improved by 22%, 6.3%, and 90% in a corresponding sequence. The optimized condition for mechanical strength and surface quality is thermal processing after hot vapour surface modification with cooling inside the hot air oven, where tensile strength, hardness (shore D), and surface roughness were noted as 50.292 N/mm2, 83, and 0.465 µm respectively, recorded a maximum tensile strength of 51.621 N/mm2 for only heat treatment with oven cooling, while minimum surface roughness of 0.372 µm for only vapour treatment. Heat treatment enhanced mechanical strength, vapour exposure improved surface smoothness, while integrated post treatment enhanced both attributes. Post-fabrication state concurrently enhance all the output factors of end-stage products created by employing fused deposition modelling, thereby increasing the overall capabilities of the AM sector.
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Authors and Affiliations

Mohd Yousuf Ali
1
ORCID: ORCID
G. Krishna Mohana Rao
1
ORCID: ORCID
B. Anjaneya Prasad
1
ORCID: ORCID

  1. Jawaharlal Nehru Technology University Hyderabad University College of Engineering Science and Technology, Department of Mechanical Engineering, Hyderabad, Telangana, India
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Abstract

This study examines the sliding wear behavior of hypoeutectic spheroidal graphite iron (SGI) and compacted graphite iron (CGI) under different thermal conditions, focusing on their potential for high-temperature tribological applications. Samples of SGI and CGI with varying magnesium content were synthesized and subjected to both rotary and linear reciprocating wear tests at temperatures ranging from room temperature to 500°C. The wear loss and frictional forces were analyzed in detail using scanning electron microscopy (SEM) and energy-dispersive X-ray spectroscopy (EDX). The results demonstrate distinct tribological responses between SGI and CGI, governed by graphite morphology and microstructural stability at elevated temperatures. CGI showed enhanced thermal stability and crack resistance due to its coral-like graphite structure, while SGI exhibited superior ducti­lity and moderate wear resistance.

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Authors and Affiliations

Venu Gopal Rao Siruvolu
1
ORCID: ORCID
Ahmed Abdullah Aafaq
2
ORCID: ORCID
Nagendra Singh
3
ORCID: ORCID
Pankaj Kumar
4
ORCID: ORCID
Akshay Ganpat Tajane
5
ORCID: ORCID
Beporam Iftekhar Hussain
6
ORCID: ORCID

  1. Department of Mechanical Engineering, DRK Institute of Science and Technology, India
  2. Department of Mechanical Engineering, B.S. Abdur Rahman Crescent Institute of Science and Technology, Vandalur, Chennai, Tamil Nadu, India
  3. Department of Mechanical Engineering, Institute of Engineering and Technology, Khandari Campus, Agra, UP, India
  4. Department of Mechanical Engineering, Chandigarh University, Punjab, India
  5. Department of Mechanical Engineering, Sandip University, Nashik, Maharashtra, India
  6. Department Mechanical Engineering, Bapatla Engineering College, Bapatla, Andhra Pradesh, India
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Abstract

This study investigates how prior heat exposure alters the low velocity impact response of glass fiber reinforced polymer laminates under a constant 16 J impact. Specimens were conditioned at 23.5°C, 50°C, 70°C, and 90°C and then tested. Peak load declined steadily with temperature from 2.040 kN at 23.5°C to 1.535 kN at 50°C to 1.52 kN at 70°C to 1.345 kN at 90°C. Contact duration showed a shallow rise followed by a drop, reported as 8.95 ms at 23.5°C, 9.10 ms at 50°C, 8.45 ms at 70°C, and 8.00 ms at 90°C. Absorbed energy decreased with heat, moving from 15.5 J at 23.5°C to 13.4 J at 50°C to 13.1 J at 70°C to 10.6 J at 90°C. Damage footprints expanded markedly with temperature, with top surface area growing from 152.36 mm2 at 23.5°C to 185.22 mm2 at 50°C to 202.47 mm2 at 70°C to 255.58 mm2 at 90°C, and bottom surface area from 100.24 mm2 to 135.66 mm2 to 155.08 mm2 to 185.09 mm2 over the same temperatures. The combined trends indicate thermally driven matrix softening and viscoelastic effects that reduce load bearing capacity and energy dissipation, shorten the effective contact window, and enlarge subsurface damage. Together these quantitative findings clarify how temperature weakens structural integrity under low velocity impact and provide design relevant guidance for material selection, allowable loads and operational safety margins in components expected to operate in elevated temperature environments, including mobility, aerospace, and energy applications.
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Authors and Affiliations

Sunith Babu Loganathan
1
ORCID: ORCID
Lokesha Krishnappa
1
ORCID: ORCID
Girish V. Kulkarni
1
ORCID: ORCID
Jaya Prakash Kode
2
ORCID: ORCID
Rajesh Mathivanan
3
ORCID: ORCID
Namburi Harsha
4
ORCID: ORCID
Rahul M. Cadambi
5
ORCID: ORCID

  1. Department of Mechanical Engineering, Ramaiah Institute of Technology, MSR Nagar, MSRIT Post, Bengaluru, 560 054, India
  2. Mechanical Engineering, VNR Vignana Jyothi Institute of Engineering and Technology, India
  3. Mechanical Engineering, PES University, India
  4. Mechanical Engineering, S.R.K.R. Engineering College (A), India
  5. Mechanical and Manufacturing Engineering, Ramaiah University of Applied Sciences, India
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Abstract

Aluminum Metal Matrix Composites (AMMCs) are well known for their superior mechanical properties and wear resistance, which makes them suitable for use in automobiles and the aerospace industry. Wear behavior, tensile strength and micro-Vickers hardness of Al 6061 reinforced with ZrB₂, produced by the stir casting process, were studied in this research. To further improve its characteristics, the composite was subjected to T4 heat treatment, consisting of solutionizing, quenching, and natural aging. Experimental findings indicated noticeable improvements in tensile strength, hardness as well as wear resistance with higher ZrB2 content. The increased hardness is due to strong interfacial bonding between Al 6061 matrix and ZrB2 particles and precipitation hardening effect due to T4 treatment. Additionally, the homogeneous dispersion of ZrB2 particles efficiently resisted material loss during wear. The results indicate that Al 6061/ZrB2 composites, especially T4-treated ones, highly suitable for applications requiring superior surface hardness and durability.
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Authors and Affiliations

Priyadarsini Morampudi
1
ORCID: ORCID
Venkata Satya Prasad Somayajula
1
ORCID: ORCID
Ravi Kumar Panthangi
2
ORCID: ORCID
Sachin S. Harak
3
ORCID: ORCID
Gianender Kajal
4
ORCID: ORCID
G. Srikar
5
ORCID: ORCID