academic projects for aeronautical students

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Topics related to CFD for Aeronautical Students. 1. CFD analysis for suppression of sloshing in spacecraft fuel tank 2. CFD analysis for diffuser of Gas turbine and related engines. 3. CFD analysis for Convergent –Divergent nozzle for prediction of normal and oblique shocks at different altitudes. 4. CFD Analysis for Nose – Cone of rocket vehicles. 5. CFD/CHT analysis for cooling of axial turbine blades. 6. CFD analysis for flow over two circular cylinders for vortex generation, mean drag co-efficient. 7. CFD analysis for wing with and without blended winglets at different cant angle. 8. CFD analysis for wing with and without feather cut winglets. 9. CFD analysis for axial flow compressor at different mass flow rates. 10. CFD analysis for Centrifugal compressor at different rpm. 11. CFD analysis for different shapes of the nozzle for flow performance. 12. CFD analysis for flow through a nozzle with addition of grooves for performance prediction. 13. CFD analysis for Anti-icing in aircraft wings. Topics related to FEA for Aeronautical Students. 1) Finite Element Analysis of Aircraft Wing 2) Stress Analysis of Nose Cone of an Aircraft 3) Design & Analysis of mounting Bulkheads

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Academic Projects for Aeronautical Students

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Topics related to CFD for Aeronautical Students. 1. CFD analysis for suppression of sloshing in spacecraft fuel tank2. CFD analysis for diffuser of Gas turbine and related engines. 3. CFD analysis for Convergent Divergent nozzle for prediction of noral and obli!ueshocks at different altitudes. ". CFD #nalysis for $ose Cone of rocket vehicles. %. CFD&C'( analysis for cooling of a)ial turbine blades. *. CFD analysis for flo+ over t+o circular cylinders for vorte) generation, ean dragco-efficient. .. CFD analysis for +ing +ith and +ithout blended +inglets at different cant angle./. CFD analysis for +ing +ith and +ithout feather cut +inglets.0. CFD analysis for a)ial flo+ copressor at different ass flo+ rates.11. CFD analysis for Centrifugal copressor at different rp. 11. CFD analysis for different shapes of the nozzle for flo+ perforance.12. CFDanalysisforflo+throughanozzle+ithadditionofgroovesforperforanceprediction.13. CFD analysis for #nti-icing in aircraft +ings.Topics related to FEA for Aeronautical Students. 1) Finite Element Analysis of Aircraft Wing2) Stress Analysis of Nose Cone of an Aircraft3) Design & Analysis of mounting Bulkea!s") FEA of #C Beam strengtene! $it F#% &aminates') FEA of A(ial Flo$ Com)ressor*) FEA of Centrifugal Flo$ Com)ressor+) Analysis of Cylin!rical Sell Fuselage Structure,) Stress Analysis of Aircraft -anger.) FEA of sort range %assenger Aircraft1/) FEA of &an!ing 0ear11) Analysis of S)lit Bla!e #u!!er12) 1o!al Analysis of 2ur3ine Bla!e Analysis13) Analysis of 0as 2ur3ine Di4user1") FEA of Aircraft Engine Nacelle