PROFILE
UPM's Staff Profile
PROF. MADYA IR. DR. MOHAMMAD YAZDI BIN HARMIN
ASSOCIATE PROFESSOR
FACULTY OF ENGINEERING
myazdi@upm.edu.my
PROFESSIONAL
Dr. Mohammad Yazdi Harmin started his career at Universiti Putra Malaysia (UPM) as a Tutor upon completion of his Bachelor of Aerospace Engineering (UPM) back in 2002. After five years of serving, he has pursued his PhD in Aeroelastic Modelling & Design at the University of Liverpool. He rejoined UPM and served as a Senior Lecturer upon completion of his PhD in 2012 and been promoted to Associate professor in 2020. He is a registered graduate engineer since 2013 and a registered professional engineer (P.Eng) since 2023 under the Board of Engineers Malaysia (BEM). He is also a founding member of Aerospace Malaysia Society which was established in 2017. His main research interests lie in the fields of Aeroelasticity (Simulation, Modelling & Testing), Swarm Intelligence and Reduced Order Model approaches. He has published over 40 journal publications and conference articles in the aforementioned topics and has received several grants from various funding agencies. As a main supervisor, he has successfully produced and supervising a number of postgraduate holders and students (Master & PhD) in various aerospace engineering sub-expertise.
NAME:
(PROF. MADYA IR. DR.) MOHAMMAD YAZDI BIN HARMIN
POSITION:
ASSOCIATE PROFESSOR
ENTITY:
FACULTY OF ENGINEERING
DOWNLOAD CURRICULUM VITAE (PDF)
FIELDS OF SUPERVISION
Aerospace Engineering / Computational Methods In Engineering / Control System Engineering / Mechanical Engineering
EDUCATIONAL BACKGROUND
2022
Bachelor of Aerospace Engineering (Honours) – University Putra Malaysia
2012
PhD (Aeroelastic Modelling & Design) – University of Liverpool
WORKING EXPERIENCE
2020
Associate Professor, Department of Aerospace Engineering, UPM
2012
Senior Lecturer, Department of Aerospace Engineering, UPM
2002
Tutor, Department of Aerospace Engineering, UPM
PUBLICATION
2024:
Fatigue Life Prediction on Critical Component for Structure Life Extension of X - Aircraft
2024:
Visualizing Partially Loosened Fastener through Frequency-Wavenumber Analysis of Ultrasonic Wavefield
2024:
Comparative Study of Fluid-Structure Interaction Approaches for High Aspect Ratio Wing Applications
2024:
High-Resolution Wavenumber Bandpass Filtering of Guided Ultrasonic Wavefield for the Visualization of Subtle Structural Flaws
2023:
Adaptive Mode Filter for Lamb Wavefield in the Wavenumber-Time Domain Based on Wavenumber Response Function
2023:
Guided ultrasonic waves propagation imaging: a review
2022:
Investigation of Modal Strain Energy for Varying Ribs Orientation Concept of Untapered Wing Box Model
2022:
Modal Analysis of Conceptual Microsatellite Design Employing Perforated Structural Components for Mass Reduction
2022:
Structural Responses of a Conceptual Microsatellite Structure Incorporating Perforation Patterns to Dynamic Launch Loads
2022:
Damage Visualization based on Frequency Shift of Single-Mode Ultrasound-Guided Wavefield
2021:
Computational Study of Mass Reduction of a Conceptual Microsatellite Structural Subassembly Utilizing Metal Perforations
2019:
Nonlinear Reduced Order Model of Rectangular High Aspect Ratio Wing with and without Follower Force Effects
2019:
Nonlinear Reduced Order Model for Aeroelastic Static Deformations of Cantilevered Rectangular High Aspect Ratio Wing Model
2018:
Parametric Study on the Flutter Characteristics of a Simple Rectangular Wing-Box Model with Varying Ribs Orientation
2018:
Nonlinear reduced order model of high aspect ratio rectangular wing plate
2018:
Preliminary investigation on experimental modal analysis of high aspect ratio rectangular wing model
2018:
Parametric study of varying ribs orientation and sweep angle of un-tapered wing box model
2018:
Aerodynamic performance of X-plane with two different types of inboard stores
2016:
The design of viterbi decoder for low power consumption space time trellis code without adder architecture using RTL model