Selamat Datang Ke
LAMAN WEB PERIBADI
Dr.
Dayang Laila Abang Haji Abdul Majid
FAKULTI KEJURUTERAAN
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PROFILE

PERSONAL PARTICULARS
SALUTATION : Dr.
NAME : Dayang Laila Binti Abang Haji Abdul Majid
POST :
DEPARTMENT : Fakulti Kejuruteraan

EDUCATIONAL BACKGROUND
  • 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


  • WORKING EXPERIENCE
  • 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.
  • Pegawai Lindungan Radiasi (Radiation Protection Officer) Dis 95-Feb 98 Komag USA (M) Sdn. (Sarawak Operations) Kuching,
    Sarawak.
  • Tutor Mac 98-Mei 2001 Jab. Kejuruteraan Aeroangkasa, Fakulti Kejuruteraan, UPM.


  • CONFERENCE / WORKSHOP / SEMINAR
  • Majid, D.L., Basri, S. and Zahari, R. Aeroelastic tailoring of woven glass/epoxy
    laminate, WEC 2007.
  • 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.
  • 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.
  • ShahNor Basri, Renuganth Varatharajoo, Dayang LailaMajid, Abdul Aziz Jaafar
    (Editors), Proceedings ofAEROTECH-2005. ISBN 983-42130-0-X, 2005.
  • 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
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.


  • AWARD AND ACHIEVEMENT
  • Gold Medal(antarabangsa)
    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.
  • 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
  • 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
  • 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
  • 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


  • AREA OF SPECIALISATION
  • ADVANCE ENGINEERING MATERIAL AND
    AEROELASTICITY


  • RESEARCH PROJECT
  • Structural optimization of an aeroelastically tailored composite wing EAR IRPA(09-02-
    04-0899EA001) 2004-2006 RM129,000
  • Characterisation of composite aircraft wing under aerodynamic loading, Skim Latihan
    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


  • PUBLICATION
  • E. Mahdi, A. S. M. Hamouda, A. S. Mukhtar and D. L. Majid. Many Aspects to improve
    damage tolerance of collapsible composite energy absorber devices, International
    Journal of Composite Structures 67/2, 2005, 175-187.
  • S.T. Taher, E. Mahdi, A.S. Mokhtar, D.L. Majid, F.R. Ahmadun, Prithvi Raj Arora. A
    new composite energy absorbing system for aircraft and helicopter, Composite
    Structures 75 (2006), 14-23.
  • Attaran, D.L. Majid, S. Basri, A.S. Mohd Rafie, and E.J. Abdullah. Structural
    optimization of an aeroelastically tailored composite flat plate made of woven
    fiberglass/epoxy, Acta Mechanica. Accepted: 18th June 2007. Published online: 3rd
    Septemb
  • DL Majid and S Basri. LCO flutter of cantilevered woven glass/epoxy laminate in
    subsonic flow, Acta Mechanica Sinica. 2008 24(1)
  • A. 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, Jurnal
    Mekanikal, Issue 22, Dec 2006.
  • Dayang Laila Majid and ShahNor Basri. A parametric aeroelastic analysis of a thin flat
    plate in subsonic flow, Journal of Industrial Technology 14(1),2005, 21-36.
  • Dayang Laila Majid, ShahNor Basri, Waqar Asrar and Faizal Mustapha, Subsonic
    Aeroelastic Analysis of A Thin flat Plate, IEM Juornal, Vol. 64,No. 2, June 2003.




  • PUBLICATION (KMPORTAL)
    Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coands Jet 2013
    The Effects of Stacking Sequence Layers of Hybrid Composite Materials in Energy Absorption under the High Velocity Ballistic Impact Conditions: An Experimental Investigation 2013
    Identification of Modal Properties of Composite Thin Plate Using OMA in Wind Tunnel Environment 2013
    Determination of Pulverized Material Permittivity for Microwave Absorber Applications 2013
    SIMULATION OF IMPACT ON COMPOSITE HEMISPHERICAL 2013
    Damage Identification and Classification in CFRP Laminates A SEM Based Study 2012
    GEOMETRIC NON-LINEAR ANALYSIS OF LAMINATED COMPOSITE PLATES USING HIGHER ORDER FINITE STRIP METHOD 2012
    Geometric Non-linear Analysis of Composite Laminated Plates using Higher Order Finite Strip Element 2012
    Damage Classification in CFRP Laminates using Principal Component Analysis (PCA) Approach 2012
    Modal Properties of a Cantilevered Laminated Woven Composite Plate as affected by Stacking Sequence and Fiber Orientation: An Experimental Study 2012
    Novitect; a novelty detection soft-computing algorithm for Structural Health Monitoring (SHM) system 2012
    A CONDITION STRUCTURAL INDEX (CSI) USING PRINCIPAL COMPONENT ANALYSIS (PCA) FOR NORMAL, DAMAGE AND REPAIR CONDITIONS OF CFRP LAMINATE 2012
    Variable Valve Timing on Piston Engine for Lightweight Aircraft 2012
    Factorial Study on the Tensile Strength of a Coir Fiber-Reinforced Epoxy Composite 2012
    Experimental Investigation of HSS Face Milling to AL6061 using Taguchi Method 2012
    Damage Identification and Classification in CFRP Laminates A SEM Based Study 2012
    Damage Classification in CFRP Laminates using Principal Component Analysis (PCA) Approach 2012
    Modal Properties of a Cantilevered Laminated Woven Composite Plate as affected by Stacking Sequence and Fiber Orientation: An Experimental Study 2012
    Novitect; a novelty detection soft-computing algorithm for Structural Health Monitoring (SHM) system 2012
    Dynamic analysis of a cantilevered woven composite plate-like wing 2012
    Effect of Fiber Orientation on the Structural Response of a Smart Composite Structure 2012
    Geometric Non-linear Analysis of Composite Laminated Plates using Higher Order Finite Strip Element 2012
    GEOMETRIC NON-LINEAR ANALYSIS OF LAMINATED COMPOSITE PLATES USING HIGHER ORDER FINITE STRIP METHOD 2012
    THERMAL POST-BUCKLING OF SHAPE MEMORY ALLOY COMPOSITE PLATES UNDER NON-UNIFORM TEMPERATURE DISTRIBUTION 2011
    Cotton reinforced biopolymer matrix composite: Effect of ultraviolet on its mechanical properties 2011
    A structural health monitoring of a pitch catch active sensing of PZT sensor on normal, damage and repair aircraft spoiler 2011
    FINITE ELEMENT ANALYSIS AND SIMULATION OF IMPACT LOADING ON ELASTIC PANEL STRUCTURE 2011
    BUCKLING AND POST-BUCKLING IMPROVEMENTS OF LAMINATED COMPOSITE PLATES USING FINITE ELEMENT METHOD 2011
    Thermal free vibration analysis of temperature-dependent functionally graded plates using second order shear deformation 2011
    Optimal sintering procedure to fabrication of functionally graded hydroxyapatite-titanium 2011
    Thermal Free Vibration Analysis of Temperature-dependent Functionally Graded Plates Using Second Order Shear Deformation 2011
    A Preliminary Study on Translational Kinetic Energy Absorption Using Coconut-fiber (Coir) Sheets as a Potential Impact-worthy Constituent in Advanced Aerospace Material 2011
    A SHM of a Pitch using PZT on aircraft spoiler 2011
    Critical Speeds for Carbon/Epoxy Composite Rotors in Spacecraft Energy 2011
    Null 2011
    Fabrication of functionally graded Hydroxyapatite- Titanium by applying optimal sintering procedure and powder metallurgy 2011
    Flutter analysis of a hybrid plate-like fiber reinforced composite wing 2011
    Free Vibration Analysis of Solar Functionally Graded Plates with Temperature-dependent Material Properties Using Second Order Shear Deformation Theory 2011
    HIGH VELOCITY IMPACT DAMAGE ANALYSIS FOR GLASS EPOXY - LAMINATED PLATES 2011
    Impact Damage Detection and Quantification for CFRP Laminates Subjected to Low Velocity Impact Damage-A NDT Approach 2011
    THERMAL POST-BUCKLING IMPROVEMENTS OF LAMINATED COMPOSITE PLATES USING USING THE ACTIVE STRAIN ENERGY TUNING APPROACH 2011
    THERMAL BUCKLING AND POST-BUCKLING IMPROVEMENTS OF LAMINATED COMPOSITE PLATES USING FINITE ELEMENT METHOD 2011
    Preliminary Review of Biocomposites Materials for Aircraft Radome Application 2011
    Parametric Study on Cohesive Element for Composite Fuselage 2011
    Optimal Sintering Procedure to Fabrication of Functionally Graded Hydroxyapatite-Titanium 2011
    Damage Effect on the modal parameters of isotropic plate 2010
    CRUSH SIMULATION OF WOVEN C-GLASS/EPOXY UNMANNED ARIAL VEHICLEFUSELAGE SECTION 2010
    Vibration Analysis of an Aluminum Aircraft Instrument Panel Board 2009
    Heat Distribution in Rectangular Fins Using Efficient Finite Element and Differential Quadrature Methods 2009
    Aeroelastic Analysis for Eagle 150b Aircraft Wing 2009
    Comparison of Optimum Finite Element Method vs. Differential Quadrature Method in Two-dimensional Heat Transfer Problem 2008
    LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow 2008
    Extended Conventional Finite Element Method vs. Differential Quadrature Method Comparison in Two-dimensional Heat Transfer Problem 2008
    Experimental Characterization and Aeroelasticity of Cantilevered Woven Glass/Epoxy Laminate 2007



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