Industry External Projects


Sl.NoReg.NoName of the StudentProject TitleOrganization
1UR11AE017BRITTO T ALIASANALYSIS OF A 8-10 KG CLASS MINI UAVAeronautical Development Establishment (ADE), Bangalore
2UR11AE082ANAGHA A M
3UR11AE070SIMON CHALAKKAL
4UR11AE067SELVAM CDYNAMIC AND AERO ELASTIC ANALYSIS OF UAV WINGNational Aerospace Laboratory (NAL), Bangalore
5UR11AE055PRABHU DROTARY WING RESEARCH AND DEVELOPMENTHindustan Aeronautics Limited (HAL), Bangalore
6UR11AE107ATLURI PREM SWAROOPLIQUID PROPULSIONDefence Research Development Laboratory (DRDL), Hyderabad
7UR11AE038JOSHUA DANIEL RAJDESIGN, DEVELOPMENT AND TESTING OF A CYCLOCOPTER.King Fahd International Airport, King Fahd Road, Dammam, Saudi Arabia
8UR10AE039TINO JOSEPHDESIGN AND SIMULATION OF WINGLET.Indian Institute of Space Science and Technology (IIST), Trivandrum
9UT12AE001SINDHANAUNSTEADY FORCE MEASUREMENT AND DATA ANALYSIS OF A SPIKED HB (HYPERVELOCITY BALLISTIC) MODEL IN SUPERSONIC FLOWDefence Research and Development Laboratory, Hyderabad, Telangana
10UR13AE007ANTONY JOSEPH VALIAVEETILCONCEPTUAL DESIGN OF ANNULAR COMBUSTION CHAMBER FOR A GAS TURBINE ENGINEHindustan Aeronautics Limited, Bangalore
11UR13AE028GOURABH SINGHCREATING A SOFTWARE TO GENERATE PRELIMINARY DATA FOR AIRCRAFT DESIGNZOHO Corporation Private limited, Kanchipuram
12UR14AE018MOHAMMED RAFIUDEEN SORBIT THEORY FOR FOURTH-ORDER ZONAL HARMONICS USING KS REGULAR ELEMENTSTeamIndus, Bangalore
13UR15AE038NEVIN PHILIPTO STUDY RELIABILITY OF DIE DESIGNSAditya Birla Hindalco, Mumbai
14UL16AE001PREMACHANDRAN GOPINATHSTRUCTURAL AND FLOW ANALYSIS OF AN AIRCRAFTIndian Space Research Organisation, Andhra Pradesh
15UR16AE003G REEMOHDESIGNING OF FLOW-METER NOZZLE AND DETERMINATION OF MASS FLOW RATEDefence Research and Development Laboratory, Hyderabad
16UR16AE006KEERTHIVASAN G BSTUDY OF INTERACTION OF S.S.L.V SUPERSONIC JET WITH THE GRINDER AND PRESSURE LOADS ON NEW COVER SLAB.Indian Space Research Organisation, Andhra Pradesh
17UR16AE010CHRIS KEVIN PDESIGN AND ANALYSIS OF A CARBONREINFORCED HAT MEMBERCentre For Air Borne System (CABS), Bengaluru
18UR16AE011VASANTHA KANESH MDESIGN AND AUTONOMOUS RUAVIITKanpur
19UR16AE013ABIJITH JDESIGN AND ANALYSIS OF RADOME COMPONENTS OF A RECONNAISSANCE AIRCRAFT-KEVLAR FIBERCentre For Air Borne System (CABS), Bengaluru
20UR16AE014MALLETI TARUN KUMARDESIGN OF ORIFICE METER & ESTIMATION OF COEFFICIENT OF DISCHARGE & INTAKE MASS FLOW RATEDefence Research and Development Laboratory, Hyderabad
21UR16AE016NIGELDETAILED DESIGN AND ANALYSIS OF NEW THRUST VECTORING CONTROL FOR A MULTIROLE SUPERSONIC COMBAT AIRCRAFTGas Turbine Research Establishment, Bengaluru
22UR16AE020J P GOKULSTUDY OF INTERACTION OF P.S.L.V SUPERSONIC JET WITH THE GRINDER AND PRESSURE LOADS ON NEW COVER SLAB.Indian Space Research Organisation, Andhra Pradesh
23UR16AE021JEROME LDESIGN AND ANALYSIS OF SUBMERGED AIR-INTAKE FOR COOLING OF AIRCRAFT ENGINEAeronautical Development Establishment, Bengaluru
24UR16AE022AFNAN M ARIEFPARAMETRIC CFD STUDIES OF THE PREFILMED AIRBAST ATOMIZER OF A GAS TURBINE COMBUSTORGas Turbine Research Establishment, Bengaluru
25UR16AE026SRIJIN SASISTRUCTURAL AND THERMAL ANALYSIS OF HIGH PRESSURE COMPRESSOR AND TURBINE FRONT SHAFT OF AERO ENGINE USING FINITE ELEMENT METHODGas Turbine Research Establishment, Bengaluru
26UR16AE028BOMMALI ANUSHASTRESS ANALYSIS OF AERO ENGINE'S HP COMPRESSOR AND TURBINE'S MAIN SHAFT USING FEMGas Turbine Research Establishment, Bengaluru
27UR16AE029JIM DANIELDESIGN AND DEVELOPMENT OF A WEATHER MONITORING NANO DRONEAFI Technology Aeromodelling and Drones Academy, Coimbatore
28UR16AE031SINI B DAVIDDESIGN OF RAISED LIP AIR INTAKE FOR COOLING OF AN UAV ENGINEAeronautical Development Establishment, Bengaluru
29UR16AE035RIKTI KIRITKUMAR PRAVASICOMPARATIVE STUDY BETWEEN DESIGNING AND ANALYSIS OF WEDGE FLOW METER AND VENTURIMETER FOR THE ESTIMATION OF THE MASS FLOW RATEDefence Research and Development Laboratory, Hyderabad
30UR16AE037MUHAMMED SHIMNADMODELLING OF AIR COOLING SCOOP DUCT FOR AIRCRAFT ENGINEAeronautical Development Establishment, Bengaluru
31UR16AE038ANUSHKA KOSHYGEOMETRIC GENERATION AND MODELING OF A CIRCULAR TO ELLIPTICAL CURVED ENGINE EXHAUSTAeronautical Development Establishment, Bengaluru
32UR16AE039SUDARSHAN K KCIRCULAR TO ELLIPTICAL VARYING AREA NOZZLE DUCT GEOMETRY GENERATION AND ANALYSISAeronautical Development Establishment, Bengaluru
33UR16AE041SAM RONALD VCURRENT PRATICES AND ANALYSIS OF SECTORIAL, CONFIGURATION OF AERO ENGINE MAIN SHAFTGas Turbine Research Establishment, Bengaluru
34UR16AE042DELVIN FELIX DNON-LINEAR STATIC ANALYSIS OF REAR BUMPER AND NOSE LANDING GEAR WITH IMPACT LOADING AND NORMAL MODESCADD Centre, Bengaluru
35UR16AE043DELVIN S SAMUELACCELERATED AGING EXPERIMENTS FOR PROGNOSTICS OF DAMAGE GROWTH IN COMPOSITE MATERIALSVikram Sarabhai Space Centre, Thiruvananthapuram
36UR16AE048JEENA SARA JOHN VARGHESECOMPARATIVE STUDY BETWEEN THE DESIGN AND ANALYSIS OF DEBIT-METER AND VENTURI-METER WITH DIFFERENT SONIC THROAT CONTOUR DESIGN.Defence Research and Development Laboratory, Hyderabad
37UR16AE053SHANKARSHNA SFLOW ANALYSIS OF VARIOUS PLANES OF HYBRID AIRCRAFT WITH DIFFERENT ANGLE OF ATTACKIndian Space Research Organisation, Andhra Pradesh
38UR16AE058GAJALA RAJO BABA FAREED NIYAZISTRESS ,THERMAL ANALYSIS AND LIFE CALCULATIONS OF HIGH PRESSURE TURBINE AND COMPRESSOR MAIN SHAFTGas Turbine Research Establishment, Bengaluru
39UR16AE061GLORY JCFD STUDIES ON THE UPSTREAM NOZZLE OF THE PREFILMING AIRBLAST ATOMIZER OF A GAS TURBINE ENGINE COMBUSTORGas Turbine Research Establishment, Bengaluru
40UR16AE065FRENO FAHAD RCOMPUTATIONAL ANALYSIS OF PRESSURE VARIATION OF SQUEEZE FILM DAMPER IN AERO-GAS TURBINE ENGINEGas Turbine Research Establishment, Bengaluru
41UR16AE067NITESH RAJDESIGNING OF A CIRCULAR TO ELLIPTICAL CONSTANT AREA NOZZLE DUCTAeronautical Development Establishment, Bengaluru
42UT16AE002ATHIRA MANIKANDANLAMINAR FLOW PREDICTION ON A ROTATING DISC USING BEZIER CURVESGas Turbine Research Establishment, Bengaluru
43URK17AE002FEBIN P VARGHESEDESIGN AND ANALYSIS OF ASCENT TRAJECTORY FROM MOON'S SURFACE TO THE MOON'S ORBITTeamIndus, Bangalore
44URK17AE003JOSHUA JSTUDY THE BEHAVIOUR OF MORPHING WINGBlack Space Research and Development, Karnataka
45URK17AE005SAJITH MON SLINEAR STATIC ANALYSIS OF NESTAINER CONTAINERSBlack Space Research and Development, Karnataka
46URK17AE009SHERBIN SAM SSTATIC ANALYSIS OF SIDE STEP OF CARBlack Space Research and Development, Karnataka
47URK17AE010AVR AKILANDESWARRIDESIGN OF FRONT SPAR WING-ROOT SEGMENT FOR A SMALL TRANSPORT AIRCRAFTBangalore Airctaft Industries Private Limited, Bangalore
48URK17AE011N.DINESHLINEAR STATIC ANALYSIS OF REAR UNDERRUN PROTECTION DEVICEBlack Space Research and Development, Karnataka
49URK17AE018I SOUZAN SUHANATO DESIGN AND ANALYZE SUITABLE TRAJECTORIES FROM MOON TO EARTHTeamIndus, Bangalore
50URK17AE023ARYA SUBHASHDESIGN OF A WING-FUSELAGE CONNECTING BRACKET FOR A TRANSPORT AIRFRAMEBangalore Airctaft Industries Private Limited, Bangalore
51URK17AE024SAM EMMANUEL ROZARIOEVALUATION OF SHAPE OF THE CUTOUT FOR THE BOTTOM SKIN IN A TRANSPORT AIRCRAFT WING STRUCTUREBangalore Airctaft Industries Private Limited, Bangalore
52URK17AE029JYOTSANA SUMANELECTRIC PROPULSION IN AIRCRAFT WITH BATTERY ENHANCEMENT TECHNOLOGY USING 3D PRINTINGBlack Space Research and Development, Karnataka
53URK17AE030VENKATESHWARANSTUDY THE BEHAVIOUR OF BUMPER GRILL BY PERFORMING LINEAR STATIC ANALYSISBlack Space Research and Development, Karnataka
54URK17AE033VIVASHVA SUNDAR SLINEAR STATIC ANALYSIS ON MOTORCYCLE SCISSOR LIFTERBlack Space Research and Development, Karnataka
55UR16AE044RUBAN RJNORMAL MODE/MODAL ANALYSIS OF REAR UNDER RUN PROTETION DEVICE (RUPD)Black Space Research and Development, Karnataka