AERONAUTICAL ANALYSIS via Experimental and Computational Approaches /

This book consists of ten chapters focusing on advanced aeronautical analysis in aircraft, helicopter, and unmanned aerial systems. The contents are divided into two parts. One is the experimental approach, and the other on computational approach. This book describes recent research projects that ha...

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Bibliographic Details
Main Authors: Norazila Othman, editor 503750, Mastura Ab. Wahid, editor 405261, Norazila Othman, contributor 503750, Mastura Ab. Wahid, contributor 405261, Md. Nizam Dahalan, contributor 208640, Shuhaimi Mansor, contributor 429541, Ibrahim Ali Madan, contributor 632772, Shabudin Mat, contributor 618557, Mazuriah Said, contributor 242812, Kushairi Amri Kasim, contributor 632773, Iskandar Shah Ishak, 1973- contributor 521953, Anas Faiz Aris, contributor 632774, Airi Ali, 1986- contributor 606655, Mohd. Nazri Mohd. Nasir, contributor 620154, Shahdan Azman, contributor 632775, Mohamad Fitri Asreen Mohd. Asri, contributor 632777, Kung, Zi Yang, contributor 632778, Istaz Fahrurazzi Nursyirwan, contributor 632779, Mohd. Hidayatullah Minhad, contributor 632780, Nik Ahmad Ridhwan Nik Mohd., contributor 404297, Teh, Soo Chwen, 1983-, contributor 592084, Ainullotfi Abdul Latif, contributor 259275, Haris Ahmad Israr Ahmad, contributor 447070, Wong, King Jye, contributor 190503
Format: text
Language:eng
Published: Johor Bahru, Johor: PENERBIT UTM PRESS, 2020
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Summary:This book consists of ten chapters focusing on advanced aeronautical analysis in aircraft, helicopter, and unmanned aerial systems. The contents are divided into two parts. One is the experimental approach, and the other on computational approach. This book describes recent research projects that have been completed by aeronautical researchers at Universiti Teknologi Malaysia. The chapters on experimental approach cover various experimental methods to solve problems for synthetic jet actuator, flow separation and tail shake phenomenon. In addition, the chapters on experimental method also cover field tests for unmanned aerial system by showing the instrumentation used. The chapters on computational approach cover modeling steps on aircraft design theory and numerical simulation. They discuss flight performance analysis, flight dynamics and control analysis using linear controller and fuzzy logic, aerodynamic analysis on hyperbolic lifting surface using computational fluid dynamics, and structural analysis of coreless spoiler using computational solid mechanics. The knowledge on analysis shown through experimental and computational methods contribute to an excellent design modeling process and improvement to existing procedures. Chapters presented in this volume could provide proofs, guidelines or references for students, researchers, and professionals in the aeronautical industries.