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bill » ball (Expand Search), hill (Expand Search), till (Expand Search)
fills » films (Expand Search), files (Expand Search), falls (Expand Search), fulls (Expand Search)
fuels » fuel (Expand Search)
fill » full (Expand Search), film (Expand Search), fall (Expand Search)
drago » draco (Expand Search), drao (Expand Search), rago (Expand Search), drugo (Expand Search), drawo (Expand Search)
dragos » dracos (Expand Search), draos (Expand Search), ragos (Expand Search), drugos (Expand Search), drawos (Expand Search)
dragon » dracon (Expand Search), draon (Expand Search), ragon (Expand Search), drugon (Expand Search), drawon (Expand Search)
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1
Aerodynamics of a wing body with different Winglet Cant Angle.
Published 2023“…Current aircraft was designed with winglet at the tip. Winglets reduce the drag and improve fuel efficiency and range. The winglets have been in use for nearly 90 years, but it have been remained fixed. …”
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Conference or Workshop Item -
2
Numerical analysis on the aerodynamic characteristics of SUV car model install with vortex generator
Published 2025“…It is feasible to improve fuel efficiency by lowering the drag force. The study focuses on the influence of a vortex generator (VG) on the aerodynamics of a sport utility vehicle (SUV) car. …”
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Article -
3
Investigation of the effects of distributed propulsion over a flying body
Published 2023“…One of the focuses in the current age is to reduce fuel consumption. Distributed propulsion systems show great potential in improving efficiency and achieving the goal of reducing fuel consumption. …”
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Final Year Project (FYP) -
4
An experimental and simulation study of chip transportation behaviour in gundrilling
Published 2017“…The experiments were conducted in vertical square tube filled with the water-glycerine solutions which have properties similar to the coolant properties with concentration of 85 % oil to 5 % oil. …”
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Thesis -
5
Numerical study of trapped vortex combustors characteristics in small ramjets
Published 2016“…The results show that the optimal cavity size that traps a vortex inside can be determined by calculating the drag coefficient. Because the designed small combustor does not have bypass air directed into the cavity, injecting all the fuel directly in the optimal cavity always leads to an overly fuel-rich condition. …”
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Thesis -
6
Determination of operating point for a propulsive wing UAV using CFD
Published 2018“…In addition, contour plots of CFD showed wake filling effect of the cross flow fan. General trends for operating points in CFD agrees with that obtained by wind tunnel testing.…”
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Final Year Project (FYP) -
7
Validation of ground effect drone
Published 2023“…Aerodynamic data including measurements of lift, drag, thrust, and other parameters will be tested, as well as an analysis of the vehicle's stability and control characteristics in both freestream and ground effect conditions. …”
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Final Year Project (FYP)