UTM Aerolab Welcome NSF Engineering Delegations SHABUDIN BIN

UTM Aerolab

Welcome NSF Engineering & Delegations

SHABUDIN BIN MAT Ph. D, P. Eng, CEng & Mimec. HE Head of Aeronautics Lab, UTM shabudin@fkm. utm. my

Acknowledgement: 1) 2) 3) 4) Ir. Mohd. Khir Bin Muhammad Prof. Dr. Mohd. Nazri Bin Jaafar Prof. Madya Dr. Ir. Shuhaimi Bin Mansor Prof. Dr. Ir. Wan Khairuddin Bin Wan Ali

UTM AEROLAB Department of Aeronautics, Automotive and Ocean Eng. Transportation Research Alliance Universiti Teknologi Malaysia

Focus Research Areas Aerodynamics Avionics & Flight Dynamics Helicopter and Wind Turbine Delta Wing Aerodynamics Automotive Aerodynamics UAV Research Crosswind and Gust Aerodynamics 6 DOF Flight Simulator Antenna and Microwave Control Law Design Aero Design & Structures UAV Design Helicopter Design Aero-structure Design Aero Propulsion Solid Rocket Motor Bio-fuel Satellite Propulsion

Cooperation and Networking SUBSONIC AERODYNAMICS TESTING ASSOCIATION (SATA)<www. sata. aero> • World-wide organization for operators/users of low speed aerodynamic testing facilities (since 1965) • Membership from all major wind tunnel facilities: DNW, Boeing, NASA, GM, Ford, NRC, Honda etc. • UTM accepted as SATA member August, 2002

Consultancy Income Generation 2015 - 2017 RM 2, 016, 171494 2, 017, 80714 2, 015, 74180 Years

Type of Consultancy Projects Wind Engineering 8% Automotive 23% Street Lantern 10% Sheet Roof 4% FEA/CFD 2% Outdoor Fitting Products 7% Roof Tiles 32% Research (other universities) 14%

Industry Incoming Projects • Proton Wind Tunnel Test of Prototype Model • Overseametal Sdn Bhd Testing of Sheet Roof: Resistance to Wind Pressure • Asia Roofing Industries Sdn Bhd Testing of Sheet Roof: Resistance to Wind Pressure • Formino Metal Sdn Bhd Testing of Sheet Roof: Resistance to Wind Pressure • Extrabuilt (M) Sdn Bhd Wind Tunnel Test of Street Lantern • MISC Berhad & Marine Technology Centre Wind Tunnel Test of Aframax FPSO Vessels • Unmanned System Technology Sdn Bhd Wind Tunnel Test of UAV Model • DR. YG Tan Jurutera Perunding Sdn Bhd Wind Resistance Test of Residential Building • Salutary Avenue Gas Turbine Filter Test

Working with Industry q Aircraft Design q Flight Systems & simulation q Vehicle Aerodynamics q Expert Service and Training q Wind Engineering Pekat Teknologi Muarlite

Working with Higher Institution

UTM Aerolab Current ……. . We need: Particle Image Velocimetry

Subsonic Wind Tunnel Facility • • • EDUCATION & TRAINING RESEARCH TESTING SERVICES Fan Diffuser Cross-leg 2 Fan & Motor Settling Chamber • Heat Exchanger • Honeycomb • 3 Screens Test Section Cross-Leg 1

TEST SECTION FLOW Parameters QUALITY Measured value Velocity Spatial Uniformity 0. 13 % Temperature spatial uniformity 0. 16 C Flow Angularity, pitch 0. 13 o Flow Angularity, Yaw 0. 13 Axial Wind Speed Gradient 0. 0003 /m Flow Angle Gradient, pitch 0. 003 /m Flow Angle Gradient, Yaw 0. 070 /m Velocity Temporal Uniformity 0. 046 % Temperature Temporal Unifermity 0. 08 C Axial Turbulence Intensity, Urms/U, 5 Hz <f<10 k. Hz 0. 037 %

Construction (Nov ’ 99)

Commission (May 2001)

Some of Wind Tunnel Activities

Facilities 1) Wind Tunnels 2) Flight Simulator 3) Aircraft Structure Rig 4) Instrumentation and Avionics 5) Propulsion Lab 6) Computational Fluid Dynamics (Fluent) 7) Finite Element (Nastran/Patran, Abacus) 8) Aircraft Design Studio

DELTA WING RESEARCH IN UTM Project Leader : Ir. Dr. Shabudin Bin Mat, CEng & P. Eng Ph. D Glasgow University To investigates the effects of propeller on the aerodynamic characteristics above a 55° sharp-edged delta wing UAV model. Current Publication: 1. 2. 3. 4. To Investigate the effects of Leading edge bluntness, Reynolds number, angle of attack, flow control techniques above VFE -2 wing Effects of synthetic jet actuator (SJA) on flow topology of blunt-edged UTM VFE-2 wing model (2017) FBG as air pressure sensors on generic UTM-LST half model (2017) Wind Tunnel Experiments on a Generic Sharp-Edge Delta Wing UAV Model (2017) The effect of edge profile on delta wing flow (2016) CFD analysis Grant/acknowledgement : 1) UTM GUP 2) MOHE 3) Aerolab UTM

Unmanned Aerial System, UAS & Nature Inspired Flight Technologies UAS flight test & performance analysis, wing tunnel testing, unsteady flight & perturbation, aerodynamics of insect flight & kinematics Dr. -Ing. M. Nazri M. Nasir, CEng Uni. of Manchester (BSc), TU Delft (Master), TU Darmstadt (Ph. D) https: //mech. utm. my/mnazri/ mnazri@mail. fkm. utm. my 011 -10845041

OPTIMIZATION OF AIRCRAFT SYSTEM RESEARCH IN UTM Kriging method Project Leader : Dr. Norazila Othman, Ph. D Tokyo Metropolitan University, Japan Efficient gobal optimization Optimize To investigates the transonic speed effects of standard dynamic model (SDM) aircraft. To investigate the effects of engine nacelle and pylon of common research model aircraft (CRM). Current Publication: 1. Prediction of aerodynamic derivatives using computational fluid dynamics (CFD) at transonic speed, 2017. 2. Development of multiobjective trajectory-optimization method and its application to improve aircraft landing, 2016. 3. Trajectory and aerodynamic control optimization of civil aircraft descent under hazard situations based on highfidelity aerodynamic database, 2016. 4. Development of digital flight motion methodology based on aerodynamic derivatives approximation, 2016. Optimization modelling Grant/acknowledgement : 1) UTM Potential Academic Grant 2) MOHE

UNSTEADY AERODYNAMICS OF AIRCRAFT & ROAD VEHICLES Nik Ahmad Ridhwan Nik Mohd, Ph. D. Uni of Liverpool, UK ridhwan@utm. my

Ir Dr Shabudin Bin Mat, CEng & P. Eng(Head of Aerolab UTM) Tel: +6 075535845 Mobile: +6 016 3143674 Fax: +6 5535997 Email: shabudin@fkm. utm. my