Manned and Unmanned Vehicles Related
- “TYTO”, Low Speed Fixed Wing MAV – ENSAE, France
- “Mini VertiGo”, VTOL MAV – ISAE, France and U. of Arizona, USA
- “MAVion”, Ground and Air VTOL MAV – ISAE, France
- “Kreno-V”, Fixed Wing UAV – GISTDA
- “BATT (VETAL)”, VTOL UAV – HG Robotics
- “HUMMING” Metal Wall Inspection Multirotor Drone – PTTEP
- “SWIFT”, Long Endurance UAV with Deept Stall Landing Capability, KU
- “K-HELIOS”, Fixed Wing Solar UAV – KU Research and Development Institute
- “ENDLESS”, Telecommunication Signal Inspection Multirotor Drone – ENDLESS
- “MARCUS-B”, VTOL UAV – Royal Thai NAVY
- “NONTRI”, VTOL UAV – Faculty of Engineering, KU
- “BUMBLE Drone”, Dual Mode Flying Car Concept, KU
- “InspDrone”, Crack Inspection Drone, KU
Wind Tunnel and Aerodynamic Testing
- Airfoil Flutter Test, Transonic Wind Tunnel, NCKU (2540)
- MAV Aerodynamic Design and Test, S6 Close Loop Low Speed Wind Tunnel 0.45mx0.45m Test Section, ENSAE SupAero, Toulouse, France (2546-2549)
- Design of high precision Force balance for MAV Test
- Wing-Propeller Interaction Test
- Design Gust Generator System and Flexible Wing Test in S6 Wind Tunnel
- Small UAV Testing, S4 Eifel Type Open Elliptic 2mx3m Jet Test Section Wind Tunnel, Toulouse, France, (2547-2551)
- Aerodynamic Characteristics Test by 6-Component Balance
- Smoke Visualization
- Fixed Wing and Ducted Fan UAVs
- Wing Tunnel Testing AIAA Course (2552)
- Evaluated and Testing of Nano-Rotor by 5-Componenent Balance, ISAE (2552)
- Design Team Member of Close Loop Wind Tunnel at ISAE, France (2552)
- Teaching, 0.30×0.30m Open Loop Wind Tunnel, KU (2553-2561)
- Aerodynamic Test Projects, 1.5mx2.0m Close Loop Wind Tunnel, RTAFA (2558-2560)
- Testing in 1mx1m Close Loop Wind Tunnel, KU (2553-present)
- Co-Axial Propeller Test
- Several Wing and UAV Tests
- Wing-Propeller Test
- Foldable Wing in High Turbulent Flow Test
- Wing In Ground Effect Test
- Testing in 2mx2m Open Loop Wind Tunnel, KU (2558-2560)
- Propeller Test at High AoA
- Tail-Sitter VTOL UAV (Vertical Phase)
- Flow Quality Control and Check of 0.6mx0.6m Open Loop Wind Tunnel, KU (2565)
- (Current) Co-Advisor of an Intern student at Virginia Tech Wind Tunnel work on the boundary layer profile observation
- (Current Project) Control Effective of Tail Sitter VTOL Wing in Vertical Phase (AFOSR Grant No. FA2386-21-1-4044)
Other
- EHIA for U-Tapao International Airport’s Runway 2, United Analyst and Engineering Consultant Co., Ltd
- Airport Carbon Footprint Level 2-3 “Reduction-Optimisation” under Airport Carbon Accreditation Airports of Thailand (AOT)
- Inspection Balloon for Explosive Area, PTTEP
- วิทยากร “หลักสูตรประกาศนียบัตร การสร้างเครื่องบินขนาดเบาพิเศษ NAX-2” โครงการจัดอบรมด้านการบิน, มหาวิทยาลัยเกษตรศาสตร์และกองทัพเรือ
- Board Committee, Consortium of Aeronautics and Space Engineering (CASE), Thailand
- Committee (Agriculture Drone), Thai Industrial Standard Institute (TISI), Thailand