MUHD RUZAIMI MAT REJAB

Dr. MUHD RUZAIMI MAT REJAB


Research Focus & Metrics

Academic Career Length

18Years (2009-Present)

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

Representative Publications

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1 April 2013 in Composites Part B: Engineering
Verified
Journal Article
Closed access
MRMUHD RUZAIMI MAT REJAB
MUHD RUZAIMI MAT REJAB
WCW.J. Cantwell
W.J. Cantwell

21 January 2019 in International Journal of Precision Engineering and Manufacturing-Green Technology
Verified
Journal Article
Closed access
PDF file
MHM. H. M. Hamdan
M. H. M. Hamdan
Januar Parlaungan SiregarJanuar Parlaungan Siregar
Januar Parlaungan Siregar
MRMUHD RUZAIMI MAT REJAB
MUHD RUZAIMI MAT REJAB
DBD. Bachtiar
D. Bachtiar
JJJ. Jamiluddin
J. Jamiluddin
CTC. Tezara
C. Tezara

1 April 2018 in Applied Thermal Engineering
Verified
Journal Article
Closed access
TYT.M. Yusof
T.M. Yusof
HIH. Ibrahim
H. Ibrahim
WAW.H. Azmi
W.H. Azmi
MRMUHD RUZAIMI MAT REJAB
MUHD RUZAIMI MAT REJAB

1 August 2018 in Defence Technology
Verified
Journal Article
Open access
AMA.A. Mohammed
A.A. Mohammed
DBD. Bachtiar
D. Bachtiar
MRMUHD RUZAIMI MAT REJAB
MUHD RUZAIMI MAT REJAB
Januar Parlaungan SiregarJanuar Parlaungan Siregar
Januar Parlaungan Siregar

30 January 2019 in International Journal of Precision Engineering and Manufacturing-Green Technology
Verified
Journal Article
Closed access
PDF file
Januar Parlaungan SiregarJanuar Parlaungan Siregar
Januar Parlaungan Siregar
JJJamiluddin Jaafar
Jamiluddin Jaafar
TCTezara Cionita
Tezara Cionita
CJChoo Chee Jie
Choo Chee Jie
DBDandi Bachtiar
Dandi Bachtiar
YAYuli Panca Asmara
Yuli Panca Asmara

3 August 2019 in Journal of Reinforced Plastics and Composites
Verified
Journal Article
Open access
PDF file
Quanjin MaQuanjin Ma
Quanjin Ma
ISIdris M Sahat
Idris M Sahat
MRMUHD RUZAIMI MAT REJAB
MUHD RUZAIMI MAT REJAB
SHShukur Abu Hassan
Shukur Abu Hassan
BZBo Zhang
Bo Zhang
MMMubin Nm Merzuki
Mubin Nm Merzuki
The study aims to investigate the effect of different infill pattern structures on the energy-absorbing characteristics of single filament wound carbon fiber-reinforced plastic tubes, single polylactic acid and hybrid carbon fiber-reinforced plastic/ polylactic acid tubes under quasi-static axial compression condition, which were fabricated using filament winding and additive manufacturing techniques. Five infill pattern structures of single polylactic acid tubes and hybrid tubes were studied and compared on their energy-absorbing characteristics, which referred to normal, triangle, square, hexagonal and tetrahedral patterns. It concluded that the effect of the infill pattern structure had a significant influence on energy-absorbing characteristics of single polylactic acid and hybrid carbon fiber-reinforced plastic/polylactic acid tubes. For pure polylactic acid tubes, the triangle infill pattern tube represented the highest values of energy absorption ( EA) of 0.75 kJ, specific energy absorption ( SEA) of 28.50 J/g, compressive strength and modulus of 69.72 MPa and 1.40 GPa, yield strength of 27.80 MPa, peak crushing force ( Fpeak) of 23.13 kN and mean crushing force ( Fmean) of 18.82 kN. For the hybrid carbon fiber-reinforced plastic/polylactic acid tube, tetrahedral infill pattern tube showed the highest values of EA with 0.99 kJ, SEA with 29.66 J/g, Fpeak with 22.68 MPa and yield strength with 29.91 MPa. Energy absorption interaction ( EAinteraction) and interaction ratio ( φe) of all specimens were evaluated, which showed that the tetrahedral infill pattern tube recorded the highest of all hybrid tubes with 259.92 J and 35.72 %. The result revealed that the tetrahedral pattern displayed better crashworthiness in terms of crushing force efficiency ( CFE), EA and SEA in the hybrid structure, which had greater potential to apply as energy absorbers. Moreover, triangle and square infill patterns of hybrid tubes provided the negative interaction effect results, which conducted lower energy-absorbing characteristics compared to individual tubes, respectively.