Mohammad Yazdi Harmin
Mohammad Yazdi Harmin
Associate Professor, Universiti Putra Malaysia
Verified email at
Cited by
Cited by
Optimization of aeroelastic composite structures using evolutionary algorithms
A Manan, GA Vio, MY Harmin, JE Cooper
Engineering Optimization 42 (2), 171-184, 2010
Aeroelastic behaviour of a wing including geometric nonlinearities
MY Harmin, JE Cooper
The Aeronautical Journal 115 (1174), 767-777, 2011
Aeroelastic tailoring of metallic wing structures
A Abdelkader, M Harmin, J Cooper, F Bron
52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2011
Use of Monte Carlo method to estimate subsystem redesign risk for complex products: aircraft redesign case study
R Varatharajoo, F Romli, MY Harmin
Aircraft Engineering and Aerospace Technology: An International Journal, 2015
Dynamic aeroelastic prediction for geometrically nonlinear aircraft
MY Harmin, JE Cooper
International Forum on Aeroelasticity and Structural Dynamics (IFASD)–2011 …, 2011
Efficient prediction of aeroelastic behaviour including geometric non-linearities
MY Harmin, JE Cooper
Proceedings of the 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural …, 2010
Aeroelastic Tailoring Using Ant Colony Optimisation
Y Harmin, J Cooper
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2009
Solvent debinding of inconel 718 fabricated via metal injection molding
MA bin Ahmad, R bin Ibrahim, ABD bin Abu Talib, MY bin Harmin
Advanced Materials Research 1133, 275-279, 2016
Parametric study on the flutter characteristics of a simple rectangular wing-box model with varying ribs orientation
MY Harmin, MS Othman, FI Romli
International Journal of Pure and Applied Mathematics 119 (15), 3771-3777, 2018
Finite element analysis of high aspect ratio wind tunnel wing model: A parametric study
NA Rosly, MY Harmin
IOP Conference Series: Materials Science and Engineering 270, 2017
Aeroelastic tailoring via ribs orientation of NASA Common Research Model
YN Chan, MY Harmin, ASM Rafie
IOP Conference Series: Materials Science and Engineering 270 (1), 012029, 2017
Effect of surface roughness on helicopter main rotor blade
WNW Rohizan, ASM Rafie, MY Harmin, CC Ciang
IOP Conf. Ser.: Mater. Sci. Eng 152, 12001, 2016
Aeroelastic effects of a simple rectangular wing-box model with varying rib orientations
MS Othman, OT Chun, MY Harmin, FI Romli
IOP Conference Series: Materials Science and Engineering 152 (1), 012009, 2016
Market potential study for standing cabin concept for domestic low-cost commercial airlines in Malaysia
FI Romli, N Dasuki, MY Harmin
IOP Conference Series: Earth and Environmental Science 30, 012012, 2016
The design of Viterbi decoder for low power consumption space time trellis code without adder architecture using RTL model
MA Abu, H Harun, MY Harmin, NIA Wahab, MKA Kadir
World Journal of Engineering, 2016
Local-overall flexural interaction of pinned-ended thin-walled I-section columns
N Yidris, MTH Sultan, MY Harmin, ASM Rafie
Applied Mechanics and Materials 564, 444-448, 2014
Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation
TK Jun, MY Harmin, FI Romli
Applied Mechanics and Materials 629, 182-188, 2014
Generation of design alternatives of vertical passenger seat for standing cabin concept in commercial transport aircraft [J]
N Dasuki, FI Romli, MY Harmin
IOP Conference Series: Materials Science and Engineering 405 (1), 2018
Size-scale effects of inboard Store-Y on X-plane model: A parametric study using CFD
MA Rahman, MY Harmin, MFS Koslan, MR Saad, FI Romli, MT Ahmad
MS&E 270 (1), 012006, 2017
Effect of low velocity impact damage on the natural frequency of composite plates
EYL Chok, D Majid, MY Harmin
IOP Conf Ser Mater Sci Eng 270, 012025-012025, 2017
The system can't perform the operation now. Try again later.
Articles 1–20