Workshop on aero-engines, design, manufacturing and testing at Zaporizhzhya National Technical University and Motor-Sich, Zaporizhzhya, Ukraine, Jul 2010.
Apprentice certification, RED-X, Jul 09.
Advanced GD&T per ASME Y14.5M-1994 from Effective Training Inc., Westland, MI, Nov 2008.
Managing Risk -Overview, from General Motors University, Finance College, Nov 07.
Process Failure Modes & Effects Analysis from Eastern Michigan University, Centre for Quality, Oct 07.
Conceptual Modelling of Civil and Military Aero-engines- Master thesis work. Jan 11 - Jun 11
Development of mathematical models for Polytropic efficiencies of engine fan, compressor and turbine stages based on statistical research.
Development of an Optimiser algorithm to work in tandem with in-house gas turbine analysis software- EVA and aero-engine dimensions software- Weico, to optimize running conditions at take-off, top-of-climb and mid-cruise points minimizing the installed SFC.
Outputs running parameters and a 2D scaled model representing the overall dimesnsions of the engine based on Entry Into Service up to year 2020 of Rolls Royce Trent Series engines.
Shell Eco-Marathon, Eurospeedway Lausitz, -ICE Urban concept category. May 10 & May 11
Carbon fibre monocoque body, custom mapped Honda GS35 engine and an in-house made super-capacitor.
Responsibilities: Design and fabrication of the front suspension, uprights, brake mounts, steering mechanism, aerodynamic analysis of the body and driving the car at the event.
Result: Swedish record of 197 km/l of 95-Gasoline.
Numerical Study of cracks in glass-fibre wind turbine blades. Apr 10 - Jun 10
Carried out in parallel with a Solid Mechanics team.
Development of blade profile using NACA 2D profiles and 3D mesh of the domain in ANSYS workbench.
Solved in CFX, to obtain the pressure distribution and wind tunnel verification using pressure probes.
Concept Hovercraft, as Bachelor of Engineering project. Jan 05 - Jun 06
Styrofoam & plywood hull, handcrafted pine wood & epoxy propeller and an innovative mechanism to bleed air at high speeds, thus reducing the lift and increasing stability of single-rotor hovercrafts.
Responsibilities: Flow calculations involving lift and thrust, fabrication of propeller, design and fabrication of hull, support frames, lift duct, thrust duct, design of skirt and overhauling of IC engines.
Result: Won the first place in the state level inter-university projects exhibition.