PROFILE
Laman Web Staf UPM
PROF. MADYA DR. DAYANG LAILA BINTI ABANG HAJI ABDUL MAJID
PROFESOR MADYA
FAKULTI KEJURUTERAAN
PROFESIONAL
NAMA :
(Prof. Madya Dr.) Dayang Laila Binti Abang Haji Abdul Majid
JAWATAN :
Profesor Madya
ENTITI :
Fakulti Kejuruteraan
LATARBELAKANG PENDIDIKAN
1. BEng (Hons) in Mechanical and Materials Engineering. UKM 1994
2. MSc in Advanced Engineering Materials. UPM 2001
3. PhD in Aerospace Engineering. UPM Submission of thesis by Nov. 2007
2. MSc in Advanced Engineering Materials. UPM 2001
3. PhD in Aerospace Engineering. UPM Submission of thesis by Nov. 2007
PENGALAMAN KERJA
Guru Sandaran Julai-Nov 1994 SMK Pending, Kuching, Sarawak.
Guru Sandaran Dis 94–April 95 SMB St. Thomas, Kuching, Sarawak.
Jurutera Proses Mei 95-Feb 98 Komag USA (M) Sdn. (Sarawak Operations) Kuching,
Sarawak.
Sarawak.
Pegawai Lindungan Radiasi (Radiation Protection Officer) Dis 95-Feb 98 Komag USA (M) Sdn. (Sarawak Operations) Kuching,
Sarawak.
Sarawak.
Tutor Mac 98-Mei 2001 Jab. Kejuruteraan Aeroangkasa, Fakulti Kejuruteraan, UPM.
PERSIDANGAN / BENGKEL / SEMINAR
Majid, D.L., Basri, S. and Zahari, R. Aeroelastic tailoring of woven glass/epoxy
laminate, WEC 2007.
laminate, WEC 2007.
Majid, D.L.A.A., Basri, S. and Harun, H. Experimental characterization and
aeroelasticity of cantilevered woven glass/epoxy laminate, Proceedings of AEROTECH
II-2007,20-21st June 2007.
aeroelasticity of cantilevered woven glass/epoxy laminate, Proceedings of AEROTECH
II-2007,20-21st June 2007.
Rafie, A.S.M, Basri, S., Attaran, A.H., Majid, D.L., Sultan, M.T.H. and Yidris, N.
Computational analysis for Eagle150B aircraft wing, Proceedings of AEROTECH II-
2007, 20-21st June 2007.
Computational analysis for Eagle150B aircraft wing, Proceedings of AEROTECH II-
2007, 20-21st June 2007.
Rafie, A.S.M, Basri, S., Attaran, A.H., Majid, D.L., Yidris, N. and Sultan, M.T.H.
Experimental analysis for Eagle 150 Baircraft wing, Proceedings of AEROTECH II-
2007, 20-21stJune 2007.
Experimental analysis for Eagle 150 Baircraft wing, Proceedings of AEROTECH II-
2007, 20-21stJune 2007.
A.S.Mohd Rafie, A.Attaran, D.L. Majid and S.Basri. Design and development of an
experimental aeroelastic test rig, Proceedings of 1st Regional Conference on Vehicle
Engineering & Technology(RIVET 06), 3-5 July, 2006.
experimental aeroelastic test rig, Proceedings of 1st Regional Conference on Vehicle
Engineering & Technology(RIVET 06), 3-5 July, 2006.
Attaran, D.L. Majid, S. Basri and A.S. Mohd Rafie. Structural optimization of an
aeroelastically tailored composite flat plate made of woven fiberglass/epoxy,
Proceedings of 1st Regional Conference on Vehicle Engineering & Technology(RIVET
06), 3
aeroelastically tailored composite flat plate made of woven fiberglass/epoxy,
Proceedings of 1st Regional Conference on Vehicle Engineering & Technology(RIVET
06), 3
ShahNor Basri, Renuganth Varatharajoo, Dayang LailaMajid, Abdul Aziz Jaafar
(Editors), Proceedings ofAEROTECH-2005. ISBN 983-42130-0-X, 2005.
(Editors), Proceedings ofAEROTECH-2005. ISBN 983-42130-0-X, 2005.
D. L. Majid, S. Basri, E. Mahdi, A.S.M. Rafie and A.Attaran. Aeroelastic Tailoring of a
composite flat plate,Proceedings of AEROTECH 2005, ISBN 983-42130-0-X,67-71.
composite flat plate,Proceedings of AEROTECH 2005, ISBN 983-42130-0-X,67-71.
S.T. Taher, E. Mahdi, D.L. Majid and F.R. Ahmadun. Design and testing of composite
energy-absorbing keel beam for general aviation aircrafts. Proceedings ofAEROTECH
2005, ISBN 983-42130-0-X, 55-60.
energy-absorbing keel beam for general aviation aircrafts. Proceedings ofAEROTECH
2005, ISBN 983-42130-0-X, 55-60.
Dayang Laila Majid, ShahNor Basri & Waqar Asrar, Preliminary Investigation of Low
speed Aeroelasiticity of Thin flat Plate, WEC ’99, Kuala Lumpur, Malaysia, 19 – 22July
1999.
speed Aeroelasiticity of Thin flat Plate, WEC ’99, Kuala Lumpur, Malaysia, 19 – 22July
1999.
ANUGERAH DAN PENCAPAIAN
Gold Medal(antarabangsa)
54th World Exhibition of Innovation, Research and NewTechnologies, Brussels, 2005.
54th World Exhibition of Innovation, Research and NewTechnologies, Brussels, 2005.
SpecialAchievementAward(antarabangsa)
Special Achievement Award from Federal Agency forIndustrial (ROSPROM) Russian
Federation; 54th WorldExhibition of Innovation, Research and NewTechnologies, Brussels,
2005.
Special Achievement Award from Federal Agency forIndustrial (ROSPROM) Russian
Federation; 54th WorldExhibition of Innovation, Research and NewTechnologies, Brussels,
2005.
Bronze medal(kebangsaan)
Elsadiq Mahdi Ahmed Saad, Siavash Talebi Taher,Dayang Laila Abang Abdul Majid,
Fakhrul-RaziAhmadun, “Composite Energy-absorbing keel beam forgeneral aviation
aircrafts”, 16th International InventionInnovation Industri
Elsadiq Mahdi Ahmed Saad, Siavash Talebi Taher,Dayang Laila Abang Abdul Majid,
Fakhrul-RaziAhmadun, “Composite Energy-absorbing keel beam forgeneral aviation
aircrafts”, 16th International InventionInnovation Industri
Bronze medal(universiti)
Dayang Laila Abang Abdul Majid, Ir. ShahNor Basri, Mohamad Saleem, El-Sadig Mahdi,
Mohd Azmin Shakraine, Abdul Hamid Attaran, “Design and optimization of a woven fiber-reinforced composite wing”, Pameran Penyelidikan Rek
Dayang Laila Abang Abdul Majid, Ir. ShahNor Basri, Mohamad Saleem, El-Sadig Mahdi,
Mohd Azmin Shakraine, Abdul Hamid Attaran, “Design and optimization of a woven fiber-reinforced composite wing”, Pameran Penyelidikan Rek
Silver medal(universiti)
Elsadiq Mahdi Ahmed Saad, Siavash Talebi Taher,Dayang Laila Abang Abdul Majid,
Fakhrul-RaziAhmadun, “Design and testing of composite energyabsorbingkeel beam for
general aviation aircrafts”,Pameran Rekacipta, Penyelid
Elsadiq Mahdi Ahmed Saad, Siavash Talebi Taher,Dayang Laila Abang Abdul Majid,
Fakhrul-RaziAhmadun, “Design and testing of composite energyabsorbingkeel beam for
general aviation aircrafts”,Pameran Rekacipta, Penyelid
Bronze medal(fakulti)
Dayang Laila Abang Abdul Majid, Ir. ShahNor Basri,Mohamad Saleem, El-Sadig Mahdi,
Mohd AzminShakraine, Abdul Hamid Attaran, “Design andoptimization of a plate-like fiberreinforced
compositewing”, Pameran Penyelidikan Fak
Dayang Laila Abang Abdul Majid, Ir. ShahNor Basri,Mohamad Saleem, El-Sadig Mahdi,
Mohd AzminShakraine, Abdul Hamid Attaran, “Design andoptimization of a plate-like fiberreinforced
compositewing”, Pameran Penyelidikan Fak
BIDANG PENGKHUSUSAN
ADVANCE ENGINEERING MATERIAL AND
AEROELASTICITY
AEROELASTICITY
PROJEK PENYELIDIKAN
Structural optimization of an aeroelastically tailored composite wing EAR IRPA(09-02-
04-0899EA001) 2004-2006 RM129,000
04-0899EA001) 2004-2006 RM129,000
Characterisation of composite aircraft wing under aerodynamic loading, Skim Latihan
Pensyarah 2003-2004 RM10,000
Pensyarah 2003-2004 RM10,000
Fretting fatigue characterization of 7075-T6, Ti-6Al-4V and BS L65 aerospace
aluminium alloys and its applications to aerospace industry. EAR IRPA (09-02-04-0446-
EA001) 2002, RM175,000
aluminium alloys and its applications to aerospace industry. EAR IRPA (09-02-04-0446-
EA001) 2002, RM175,000
PENERBITAN
2021:
Unsteady squeezing fow of Cu‑Al2O3/water hybrid nanofuid in a horizontal channel with magnetic feld
2021:
Accurate position control of shape memory alloy actuation using displacement feedback and self-sensing system
2021:
A case study of English language Teachers perceptions towards secondary schools Students performance in the English language
2021:
Flapping actuation using temperature feedback control of coated shape memory alloy actuators
2021:
Research summary on the processing, mechanical and tribological properties of aluminium matrix composites as effected by fly ash reinforcement
2021:
Impacts of Volume of Carbon Nanotubes on Bending for Carbon- Kevlar Hybrid Fabrics
2020:
Tensile behavior of multilayer 3D smart woven composites embedded with shape memory alloy (SMA) wires
2020:
Design Fabrication of Adaptive Wing Structure
2020:
Prediction of fatigue life of aluminum 2024-T3 at low temperature by finite element analysis
2020:
Mathematical modeling and analysis of tribological properties of AA6063 aluminium reinforced with fly ash by using response surface methodology
2020:
EFFECTS OF VOLUME OF CARBON NANOTUBES ON THE ANGLED BALLISTIC IMPACT FOR CARBON KEVLAR HYBRID FABRICS