Article |
2021 |
Experimental study on the mean flow characteristics of a supersonic multiple jet configuration. Journal of Aerospace Science & Technology
, 108
(2021)
pp.1-13
|
2020 |
Aerodynamics of symmetric permeable airfoils and wings: CFD simulation. Progress in Computational Fluid Dynamics
, 20
(6)
pp.349-361
|
2020 |
Effect of a directionally porous wing tip on tip vortex. Journal of Applied Fluid Mechanics
, 13
(2)
pp.651-665
|
2019 |
A comparative study of two different numerical schemes for the simulation of nonlinear dynamics of heated falling thin films. International Journal of Recent Technology and Engineering
, 7
(6)
pp.100-105
|
2019 |
Effects of bio-inspired surface roughness on a swept back tapered NACA 4412 wing. Journal of Aerospace Technology and Management
, 11
pp.e1719
|
2019 |
An Investigation of RANS simulations for swirl-stabilized
isothermal turbulent flow in a gas turbine burner. CFD Letters
, 11
(9)
pp.14-31
|
2018 |
Aerodynamics of porous airfoils and wings. Acta Mechanica
, online 1st
pp.1-19
|
2018 |
Experimental investigation of a new spiral wingtip. International Journal of Aviation, Aeronautics, and Aerospace
, 5
(2)
pp.1-32
|
2018 |
Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing. International Journal of Aviation, Aeronautics, and Aerospace
, 5
(1)
pp.1-27
|
2018 |
Low-cost base drag reduction technique. International Journal of Mechanical Engineering and Robotics Research (IJMERR)
, 7
(4)
pp.428-432
|
2017 |
Literature review : Biomimetic and conventional aircraft wing tips. International Journal of Aviation, Aeronautics, and Aerospace
, 4
(2)
pp.1-25
|
2017 |
Yawing force of electric trimmers of a hybrid buoyant aerial vehicle. Pertanika J Sci and tech
, 25
(1)
pp.293-302
|
2017 |
Arbitrary Lagrangian-Eulerian form of flowfield dependent variation method for fluid-structure interaction application. ARPN Journal of Engineering and Applied Sciences
, 12
(7)
pp.2338-2344
|
2017 |
Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing. Measurement: Journal of the International Measurement Confederation
, 99
pp.1-6
|
2017 |
Wind tunnel testing of hybrid buoyant aerial vehicle. Aircraft Engineering and Aerospace Technology
, 89
(1)
pp.99-105
|
2017 |
Defining reference area for prediction of aerodynamic coefficients of a biologically inspired hybrid buoyant vehicle. Unmanned Systems
, 5
(4)
pp.237-246
|
2017 |
Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands. Journal of Aviation Technology and Engineering
, 6
(2)
pp.80-88
|
2016 |
Estimation of pitching moment of a hybrid lifting fuselage - Disguised as hull of an airship. ARPN Journal of Engineering and Applied Sciences
, 11
(4)
pp.2217-2221
|
2016 |
Framework of conceptual design methodology for hybrid buoyant
aircraft. Aerotecnica Missili & Spazio = The Journal of Aerospace Science, Technology and Systems
, 95
(2 (April-June))
pp.99-110
|
2016 |
A review on aerodynamics of nonflapping bird wings. Journal of Aerospace Technology and Management
, 8
(1 (Jan-Mar))
pp.7-17
|
2016 |
Wind tunnel testing on a generic model of a hybrid lifting hull. Journal of Aerospace Technology and Management
, 8
(4)
pp.467-474
|
2016 |
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft. International Journal of Unmanned Systems Engineering
, 4
(1)
pp.11-22
|
2016 |
Influence of a reverse delta-type add-on device on wake vortex alleviation. AIAA Journal
, 54
(2)
pp.625-636
|
2016 |
Assessment of engine's power budget for hydrogen
powered hybrid buoyant aircraft. Propulsion and Power Research
, 5
(1)
pp.34-44
|
2016 |
Establishing the analytical relationships for mass and volumetric mass fractions for hybrid buoyant aircraft. ARPN Journal of Engineering and Applied Sciences
, 11
(1)
pp.286-291
|
2016 |
Solutions of higher order boundary value problems by homotopy perturbation method. Malaysian Journal of Mathematical Sciences
, 10
(Special Issue)
pp.373-387
|
2016 |
Impact of a reverse delta type add-on device on the flap-tip vortex of a wing. International Journal of Aviation, Aeronautics, and Aerospace
, 3
(3)
pp.1-28
|
2015 |
Higher-Order Compact-Flow Field-Dependent Variation (HOC-FDV) method for solving two-dimensional navier-stokes equations. International Journal for Computational Methods in Engineering Science and Mechanics
, 16
(4)
pp.256-263
|
2015 |
Design and fabrication of a winged hybrid airship model for IIUM-LSWT. Advanced Materials Research
, 1115
pp.513-516
|
2015 |
The multistage homotopy perturbation method for solving chaotic and hyperchaotic Lü system. Abstract and Applied Analysis
, 2015
pp.398027-1
|
2015 |
Cambered profile of a California sea lion's body. The Journal of Experimental Biology
, 218
pp.1270-1271
|
2015 |
Flowfield-dependent variation method for moving-boundary problems. AIAA Journal
, 53
(4)
pp.1026-1036
|
2015 |
Numerical study of effect of spoiler configuration on
wake vortex alleviation. ASCE Journal of Aerospace Engineering
, 28
(3)
|
2015 |
A numerical investigation of explicit pressure-correction projection methods for incompressible flows. Engineering Applications of Computational Fluid Mechanics
pp.1-16
|
2015 |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach. IIUM Engineering Journal
, 16
(1)
pp.9-17
|
2015 |
Flowfield dependent variation method for one dimensional stationary and moving boundary problems. International Journal of Computational Science and Engineering
, 10
(1/2)
pp.130-144
|
2015 |
Half model testing for canard of a hybrid buoyant aircraft. International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering
, 9
(10)
pp.1544-1547
|
2014 |
Passive drag reduction of square back road vehicles. Journal of Wind Engineering and Industrial Aerodynamics
, 134
(2014)
pp.30-43
|
2014 |
Review of passive drag reduction techniques for bluff road vehicles.. IIUM Engineering Journal
, 15
(1)
pp.61-69
|
2013 |
A BGK-based two-equation turbulence model algorithm for solving compressible navier-stokes equations. CFD Letters
, 6
(2)
pp.46-61
|
2013 |
Two-dimensional flow properties of micronozzle under varied isothermal wall conditions . International Journal of Engineering Systems Modelling and Simulation
, 5
(4)
pp.174-180
|
2013 |
The multistage Adomian Decomposition Method for solving chaotic Lü System. Middle-East Journal of Scientific Research
, 13
pp.43-49
|
2012 |
Evolution of NACA23012 wake vortices structure using PIV . Journal of Aerospace Engineering
, 25
(1)
pp.10-20
|
2012 |
Micropump modeling: current status and challenges. Australian Journal of Basic and Applied Sciences
, 6
(1)
pp.134-142
|
2012 |
Investigation of aerodynamic parameters of a hybrid airship. Journal of Aircraft
, 49
(2)
pp.658-661
|
2011 |
Design process involved in developing mechanism of linear motor operated multiple spray operations spray gun. Australian Journal of Basic and Applied Sciences
, 5
(7)
pp.843-850
|
2011 |
Study of the reverse delta wing. Journal of Aircraft
, 48
(1)
pp.277-286
|
2011 |
Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC). Aerospace Science and Technology
, 15
(7)
pp.555-566
|
2010 |
A high order compact-flowfield dependent variation (HOC-FDV)method for inviscid flows. International Journal for Computational Methods in Engineering Science and Mechanics
, 11
(5)
pp.258-263
|
2010 |
Induced rolling moment for NACA4412 plain and flapped wing. International Journal of Aircraft Engineering and Aerospace Technology
, 82
(1)
pp.23-32
|
2010 |
Influence of differential spoiler settings on the wake the vortex characterization and alleviation. Journal of Aircraft
, 47
(5)
pp.1728-1738
|
2010 |
Higher order compact-flowfield dependent variation (HOC-FDV) solution of one-dimensional problems. Engineering Applications of Computational Fluid Mechanics
, 4
(3)
pp.434-440
|
2010 |
Influence of differential spoiler settings on the wake vortex
characterization and alleviation. Journal of Aircraft
, 47
(5)
pp.1728-1738
|
2009 |
Accuracy of Bhatnagaar-Gross-Krook scheme in solving laminar viscous flow problems. AIAA Journal
, 47
(4)
pp.885-892
|
2009 |
Experimental investigation of plain- and flapped-wing tip vortices. Journal of Aircraft
, 46
(1)
pp.254-262
|
2009 |
Comparison of high-order accurate schemes for solving the nonlinear viscous burgers equation. Australian Journal of Basic and Applied Sciences
, 3
(3)
pp.2535-2543
|
2006 |
Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting. International Journal of Numerical Methods for Heat & Fluid Flow
, 16
(1)
pp.107-120
|
2006 |
Application of Gas-Kinetic BGK Scheme for Solving 2-D Compressible Inviscid Flow around Linear Turbine Cascade. International Journal for Computational Methods in Engineering Science and Mechanics
, 7
(6)
pp.403-410
|
2005 |
Hypersonic flow simulation by the gas-kinetic bhatnagar-gross-krook scheme. AIAA JOURNAL
, 43
(7)
pp.1427-1433
|
1998 |
Chaos in wraparound fin projectile motion. AIAA Journal
, 21
(2)
pp.354-356
|
Conference or Workshop Item |
2020 |
Position of static cylinder effect on base flows.
In: 1st International Conference on Data Science, Machine Learning and Applications, 2019
|
2018 |
Passive control of base pressure with static cylinder at supersonic flow.
In: 1st International Conference on Aerospace and Mechanical Engineering (AeroMech 2017)
|
2018 |
Classical equivalent circuit characterization for a double-layer capacitor.
In: 4th IEEE International Conference on Smart Instrumentation, Measurement and Applications (ICSIMA) 2017
|
2018 |
Nonlinear dynamics of heated falling films under the influence of long-range Van Der Walls intermolecular force interactions.
In: 4th International Conference on Mechanical, Automotive, and Aerospace Engineering 2018 (ICMAAE’18)
|
2018 |
Active control of base pressure with counter clockwise rotating cylinder at Mach 2.
In: 4th IEEE International Conference on Engineering Technologies and Applied Sciences, ICETAS 2017
|
2018 |
Counter clockwise rotation of cylinder with variable position to control base flows.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
|
2018 |
The multistage homotopy perturbation method for solving hyperchaotic Chen system.
In: 4th International Conference on Mathematical Applications in Engineering 2017, ICMAE 2017
|
2017 |
Structural design of hybrid buoyant aircraft's model for subsonic wind tunnel testing.
In: 14th International Bhurban Conference on Applied Sciences & Technology (IBCAST)
|
2017 |
Instabilities in non-isothermal falling thin film flows.
In: 4th International Conference of Mathematical Applications in Engineering 2017 (ICMAE 2017)
|
2017 |
Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing.
In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16)
|
2017 |
Numerical simulation of non-isothermal thin liquid film flow on
inclined plane using an implicit finite difference scheme.
In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16)
|
2017 |
Generation of atmospheric boundary layer in the IIUM low speed wind tunnel.
In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16)
|
2016 |
A novel technique to neutralize the Yawing moment due to asymmetric thrust in a hybrid buoyant aircraft.
In: 10th International Conference on Experimental Fluid Mechanics, EFM 2015
|
2016 |
A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft.
In: 6th International Conference on Industrial Engineering and Operations Management in Kuala Lumpur, IEOM 2016
|
2016 |
Comparison of data correction methods for blockage effects in semispan wing model testing.
In: "10th International Conference on Experimental Fluid Mechanics, EFM 2015"
|
2016 |
Effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft.
In: 2015 International Conference on Mechanical Engineering and Electrical Systems (ICMES 2015)
|
2015 |
Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft.
In: 8th Ankara International Aerospace Conference 2015
|
2015 |
Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
.
In: 8th Ankara International Aerospace Conference
|
2015 |
Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed.
In: 62nd Canadian Aerospace Institute Conference (Aero 2015)
|
2015 |
Establishing the analytical relationships for mass and volumetric mass fractions for hybrid boyant aircraft.
In: International Postgraduate Conference on Engineering Research (IPCER) 2015
|
2015 |
Hydrostatic and hydrodynamic characteristics of swimming animals: an inspiration for hybrid buoyant aircraft.
In: 4th International Scientific Conference on Applied Sciences and Engineering (4 thISCASE-2015)
|
2014 |
Arbitrary Lagrangian-Eulerian Form of Flowfield
Dependent Variation (ALE-FDV) Method for 3D Problems.
In: 22nd Annual Conference of the CFD Society of Canada
|
2014 |
Conceptual design of a winged hybrid airship.
In: 21st Lighter than Air Technology Conference, Aviation 2014
|
2014 |
Stability and takeoff ground roll issues of hybrid buoyant aircraft.
In: 5TH INTERNATIONAL CONFERENCE ON MECHANICAL AND MANUFACTURING ENGINEERING 2014 (ICME2014)
|
2014 |
Comparison of digital DATCOM and wind tunnel data of a winged hybrid airship’s generic model.
In: AEROTECH V
|
2014 |
Arbitrary lagrangian-eulerian form of flowfield dependent variation method for moving boundary problems.
In: Aviation 2014 - 32nd AIAA Applied Aerodynamics Conference 2014
|
2014 |
Static longitudinal stability of a hybrid airship.
In: 11th International Bhurban Conference on Applied Sciences & Technology (IBCAST)
|
2013 |
Hybrid numeric-analytic method for solving chaotic system.
In: IIUM Research, Invention and Innovation Exhibition (IRIIE) 2013
|
2013 |
Experimental investigation of a vertical round free turbulent jet.
In: 2nd International Conference on Mechanical, Automotive and Aerospace Engineering 2013
|
2012 |
Numerical investigation of the vortical flow over delta wing and reverse delta wing.
In: 6th International Conference on Advanced Computational Engineering and Experimenting (ACE-X2012)
|
2012 |
Numerical analysis of FDV method for one-dimensional Euler equations.
In: 2nd International Conference on Mathematical Applications in Engineering (ICMAE2012)
|
2012 |
The modified Adomian decomposition method for solving
Chaotic Lü system.
In: International Conference on Mathematical Application in Engineering (ICMAE 2012)
|
2012 |
Passive drag reduction for green design.
In: International Conference on Dessign and Concurrent Engineering, 2012
|
2011 |
Improving the efficiency of micronozzle by heated sidewalls.
In: 4th International Meeting of Advances in Thermofluids (IMATT 2011)
|
2011 |
Aerodynamics of a hybrid airship.
In: 4th International Meeting of Advances in Thermofluids (IMATT 2011)
|
2011 |
Estimation of aerodynamic parameters of IIUM hybrid airship.
In: International Conference on Mechanical, Automotive and Aerospace Engineering
|
2011 |
Highly accurate compact flowfield dependent variation method for solving two-dimensional navier-stokes equations.
In: International Conference on Mechanical, Automotive and Aerospace Engineering 2011
|
2011 |
Investigation of the vortical flow around a reverse delta wing.
In: International Conference on Mechanical, Automotive and Aerospace Engineering 2011 (ICMAAE11)
|
2011 |
The accuracy of the gas-kinetic BGK finite difference
method for solving 3-D compressible inviscid flows.
In: International MultiConference of Engineers and Computer Scientists 2011 (IMECS 2011),
|
2011 |
Two-dimensional flow properties of micronozzle under varied isothermal wall conditions.
In: International Conference on Mechanical, Automotive and Aerospace Engineering, ICMAAE’11
|
2010 |
Long wave instabilities of heated falling films: role of Van Der Waals attraction.
In: XIVth International Conference Surface Forces
|
2010 |
Experimental investigation of the vortical flow around a reverse delta wing using PIV.
In: Experimental Fluid Mechanics 2010
|
2010 |
Development of the IIUM hybrid airship .
In: 3rd Engineering Conference on Advancement in Mechanical and Manufacturing for Sustainable Environment
|
2010 |
Higher order compact-flowfield dependent variation (HOCFDV)
method for solving navier-stokes equations.
In: The 8th Asian Computational Fluid Dynamics Conference
|
2010 |
Span load modification via differential spoiler setting .
In: 2010 RAeS Aerodynamics Conference Applied Aerodynamics: Capabilities and Future Requirements
|
2010 |
Development of a fuel efficient hybrid engine towards green technology.
In: International Conference on Sustainable Mobility 2010
|
2009 |
Accurate compact flowfield-dependent variation method for compressible Euler equations.
In: International Conference on Applications and Design in Mechanical Engineering 2009 (iCADME 2009)
|
2009 |
Evaluation of aircraft wing-tip vortex using PIV.
In: The 10th Asian International Conference on Fluid Machinery (AICFM)
|
2009 |
Experimental investigation of wing tip vortex.
In: 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition 2009
|
2009 |
Reynolds averaged navier-stokes flow computation of RAE2822 airfoil using gas-kinetic BGK Scheme.
In: International MultiConference of Engineers and Computer Scientists (IMECS)
|
2008 |
A gas-kinetic BGK solver for two-dimensional turbulent compressible flow.
In: International Conference on Scientific Computing
|
2008 |
The IIUM low speed wind tunnel.
In: 2nd Engineering Conference on Sustainable Engineering Infrastructures Development & Management
|
2008 |
Flow field characteristics of the IIUM low speed wind tunnel.
In: 3rd International Symposium on Advanced Fluid/Solid Science and Technology in Experimental Mechanics
|
2008 |
Natural convection heat transfer in nanofluids - a numerical study.
In: Proceedings of the 7th Symposium on Transport Phenomenon in Manufacturing Processes 2008
|
2004 |
The Efficiency of Gas-Kinetic BGK scheme for solving 2-d compressible inviscid regular shock reflection problem.
In: European Congress on Computational Methods in Applied Sciences and Engineering
|