Dr. Ing. Mochammad Agoes Moelyadi, ST., MSc.
Associate Professor
Ph.D., Technical University of Munich (TUM), Chair of Aerodynamics and Fluid Mechanics, Department of Mechanical Engineering (2006)
MSc, Cranfield University, College of Aeronautics (1998)
BSc, Institut Teknologi Bandung, Aeronautics and Astronautics (1993)
e-mail: moelyadi[at]ftmd.itb.ac.id
ITB profile: https://www.itb.ac.id/staf/profil/mochammad-agoes-moelyadi
Short Biography
Mochammad Agoes Moelyadi was born in Surakarta (Indonesia) in 1968. He is presently an associate professor and leader of Flight Physics research group in the Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung (ITB). He received his B.Sc degree from Institut Teknologi Bandung in 1993 and then worked as an aerodynamic configuration engineer at PT. Industri Pesawat Terbang Nusantara (now PT. Dirgantara Indonesia) involved in aerodynamics wing designs of N-250 and N-2130 aircrafts. In 1995-1997, he spent his time for studying aerodynamics and computational fluid dynamics in college of Aeronautics Nusantara Aircraft Industry (Now Indonesian Aerospace Industry) Nusantara Aircraft Industry (Now Indonesian Aerospace Industry), Cranfield university supported by the British Aerospace (Bae) scholarship (cooperation between BAE and PT. IPTN). In 1999, Moelyadi joined as a junior lecturer at Department of Aerospace Engineering, ITB, assisted to deliver aircraft aerodynamics and computational fluid dynamics courses and conducted a research in CFD development of 2-D High Lift Devices.
In the mid 2002, he joined as a scientific researcher in the program of the German Collaborative Research Center SFB 253 : Fundamentals of Space Plane Design. From this research, he continued to obtain a Dr.-Ing. in Hypersonic Aerodynamics and defended his doctoral research in September 2006. During the time he was also as a research assistant in aerodynamics of flapping wing. In 2009, he was back to TUM for postdoctoral research. He teaches several courses on compressible aerodynamics, advanced compressible flow and computational fluid dynamics courses. His research interests include (1) fluid structure interactions in flexible wings of HALE UAV and in flapping wing MAV, (2) High speed aerodynamics design for supersonic wind tunnel, supersonic intake and supersonic vehicle configuration, (3) numerical code of grid based High order numerical algorithm, and (4) Non-Aeronautics aero-gas dynamics related applications.