This book consists of selected peer-reviewed papers from the 2nd International Seminar on Aeronautics and Energy (ISAE 2022) focusing on the theme to revive the aviation industry post-COVID-19 pandemic. The topics discussed in this book include aircraft design and optimization, computational fluid dynamics (CFD) simulation and experimental aerodynamics, aircraft structure and aeroelasticity, guidance control and navigation, aircraft manufacturing and health monitoring avionics and system integration of UAV/drones, SITL AND HITL application on drones, rockets and missile, industrial wind…mehr
This book consists of selected peer-reviewed papers from the 2nd International Seminar on Aeronautics and Energy (ISAE 2022) focusing on the theme to revive the aviation industry post-COVID-19 pandemic. The topics discussed in this book include aircraft design and optimization, computational fluid dynamics (CFD) simulation and experimental aerodynamics, aircraft structure and aeroelasticity, guidance control and navigation, aircraft manufacturing and health monitoring avionics and system integration of UAV/drones, SITL AND HITL application on drones, rockets and missile, industrial wind engineering, green fuel and aviation sustainability, and aviation management. This book is a valuable resource for academicians and industry players in the field of aviation and sustainability.Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Dr. Nik Ahmad Ridhwan Nik Mohd. is Senior Lecturer in the Department of Aeronautics, Automotive and Naval Engineering in the Faculty of Mechanical Engineering at Universiti Teknologi Malaysia in Johor, Malaysia. He holds a Bachelor of Engineering and a Master of Engineering in Mechanical Engineering from UTM Johor, Malaysia, as well as a Doctor of Philosophy in Mechanical Engineering from the University of Liverpool, the UK. His areas of interest in study include aerodynamics, computational fluid dynamics, and renewable energy. He has published numerous articles in peer-reviewed international and national journals. He has been actively involved in research initiatives mostly financed by the governments of Malaysia and currently funded by Japan Government. He had also completed more than ten industrial consulting projects. Associate Professor Dr. Ir. Shabudin Bin Mat obtained his Bachelor of Aerospace Engineering from UTM, Malaysia, in 1997. He then continued his Master inENSICA, France, in 1998. He obtained his Ph.D. in low-speed aerodynamics from the University of Glasgow in 2010. He was in the VFE-2 panel from 2005 to 2010 where he was introduced to delta wing aerodynamics. He has published more than 80 papers in the field of aerodynamics of delta wing. He is currently supervising students in experimental aerodynamics and wind engineering. Currently he is Director of UTM Aerolab, one of UTM Centres of excellent. Dr. Shabudin Bin mat also is Registered Professional Engineer with Malaysian Board of Engineer (BEM) and United Kingdom Chartered Engineers.
Inhaltsangabe
Experimental Studies of the Effect of Rectangular-Shaped Canard on a Generic Blended Wing Body (BWB).- Blowing Active Flow Control on FFA-W3-270 Airfoil Model.- Experimental Investigation of a Generic Light Aircraft Model with Dual External Stores.- Computational Analysis on Aerodynamics of a Boxfish-Inspired Airship.- Computational Fluid Dynamics Analysis of High Aspect Ratio Wing Application.- Effect of Surface Roughness Size on the Skin Friction Drag for NACA 0012 Airfoil.- Noise Estimation of NACA 0012 Airfoil Using DES Method.- Numerical Study of Air-Intake Performance of a Scramjet with Various Cowl Lip Length.- Design and Numerical Study of High-Speed Water Tunnel with Interchangeable Test Section.- Avionics and System Integration on UAV/Drone.- Development of an Autonomous RC Catamaran for Surveillance and Pollution Monitoring.- Development of Autonomous Battery Charging Station for Campus Surveillance UAV.- Preliminary Development and Performance Testing of an Autonomous Battery Charging System for a Two Legs Multicopter.
Experimental Studies of the Effect of Rectangular-Shaped Canard on a Generic Blended Wing Body (BWB).- Blowing Active Flow Control on FFA-W3-270 Airfoil Model.- Experimental Investigation of a Generic Light Aircraft Model with Dual External Stores.- Computational Analysis on Aerodynamics of a Boxfish-Inspired Airship.- Computational Fluid Dynamics Analysis of High Aspect Ratio Wing Application.- Effect of Surface Roughness Size on the Skin Friction Drag for NACA 0012 Airfoil.- Noise Estimation of NACA 0012 Airfoil Using DES Method.- Numerical Study of Air-Intake Performance of a Scramjet with Various Cowl Lip Length.- Design and Numerical Study of High-Speed Water Tunnel with Interchangeable Test Section.- Avionics and System Integration on UAV/Drone.- Development of an Autonomous RC Catamaran for Surveillance and Pollution Monitoring.- Development of Autonomous Battery Charging Station for Campus Surveillance UAV.- Preliminary Development and Performance Testing of an Autonomous Battery Charging System for a Two Legs Multicopter.
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