| 1 | UR11AE017 | BRITTO T ALIAS | ANALYSIS OF A 8-10 KG CLASS MINI UAV | Aeronautical Development Establishment (ADE), Bangalore |
| 2 | UR11AE082 | ANAGHA A M |
| 3 | UR11AE070 | SIMON CHALAKKAL |
| 4 | UR11AE067 | SELVAM C | DYNAMIC AND AERO ELASTIC ANALYSIS OF UAV WING | National Aerospace Laboratory (NAL), Bangalore |
| 5 | UR11AE055 | PRABHU D | ROTARY WING RESEARCH AND DEVELOPMENT | Hindustan Aeronautics Limited (HAL), Bangalore |
| 6 | UR11AE107 | ATLURI PREM SWAROOP | LIQUID PROPULSION | Defence Research Development Laboratory (DRDL), Hyderabad |
| 7 | UR11AE038 | JOSHUA DANIEL RAJ | DESIGN, DEVELOPMENT AND TESTING OF A CYCLOCOPTER. | King Fahd International Airport, King Fahd Road, Dammam, Saudi Arabia |
| 8 | UR10AE039 | TINO JOSEPH | DESIGN AND SIMULATION OF WINGLET. | Indian Institute of Space Science and Technology (IIST), Trivandrum |
| 9 | UT12AE001 | SINDHANA | UNSTEADY FORCE MEASUREMENT AND DATA ANALYSIS OF A SPIKED HB (HYPERVELOCITY BALLISTIC) MODEL IN SUPERSONIC FLOW | Defence Research and Development Laboratory, Hyderabad, Telangana |
| 10 | UR13AE007 | ANTONY JOSEPH VALIAVEETIL | CONCEPTUAL DESIGN OF ANNULAR COMBUSTION CHAMBER FOR A GAS TURBINE ENGINE | Hindustan Aeronautics Limited, Bangalore |
| 11 | UR13AE028 | GOURABH SINGH | CREATING A SOFTWARE TO GENERATE PRELIMINARY DATA FOR AIRCRAFT DESIGN | ZOHO Corporation Private limited, Kanchipuram |
| 12 | UR14AE018 | MOHAMMED RAFIUDEEN S | ORBIT THEORY FOR FOURTH-ORDER ZONAL HARMONICS USING KS REGULAR ELEMENTS | TeamIndus, Bangalore |
| 13 | UR15AE038 | NEVIN PHILIP | TO STUDY RELIABILITY OF DIE DESIGNS | Aditya Birla Hindalco, Mumbai |
| 14 | UL16AE001 | PREMACHANDRAN GOPINATH | STRUCTURAL AND FLOW ANALYSIS OF AN AIRCRAFT | Indian Space Research Organisation, Andhra Pradesh |
| 15 | UR16AE003 | G REEMOH | DESIGNING OF FLOW-METER NOZZLE AND DETERMINATION OF MASS FLOW RATE | Defence Research and Development Laboratory, Hyderabad |
| 16 | UR16AE006 | KEERTHIVASAN G B | STUDY 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 |
| 17 | UR16AE010 | CHRIS KEVIN P | DESIGN AND ANALYSIS OF A CARBONREINFORCED HAT MEMBER | Centre For Air Borne System (CABS), Bengaluru |
| 18 | UR16AE011 | VASANTHA KANESH M | DESIGN AND AUTONOMOUS RUAV | IITKanpur |
| 19 | UR16AE013 | ABIJITH J | DESIGN AND ANALYSIS OF RADOME COMPONENTS OF A RECONNAISSANCE AIRCRAFT-KEVLAR FIBER | Centre For Air Borne System (CABS), Bengaluru |
| 20 | UR16AE014 | MALLETI TARUN KUMAR | DESIGN OF ORIFICE METER & ESTIMATION OF COEFFICIENT OF DISCHARGE & INTAKE MASS FLOW RATE | Defence Research and Development Laboratory, Hyderabad |
| 21 | UR16AE016 | NIGEL | DETAILED DESIGN AND ANALYSIS OF NEW THRUST VECTORING CONTROL FOR A MULTIROLE SUPERSONIC COMBAT AIRCRAFT | Gas Turbine Research Establishment, Bengaluru |
| 22 | UR16AE020 | J P GOKUL | STUDY 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 |
| 23 | UR16AE021 | JEROME L | DESIGN AND ANALYSIS OF SUBMERGED AIR-INTAKE FOR COOLING OF AIRCRAFT ENGINE | Aeronautical Development Establishment, Bengaluru |
| 24 | UR16AE022 | AFNAN M ARIEF | PARAMETRIC CFD STUDIES OF THE PREFILMED AIRBAST ATOMIZER OF A GAS TURBINE COMBUSTOR | Gas Turbine Research Establishment, Bengaluru |
| 25 | UR16AE026 | SRIJIN SASI | STRUCTURAL AND THERMAL ANALYSIS OF HIGH PRESSURE COMPRESSOR AND TURBINE FRONT SHAFT OF AERO ENGINE USING FINITE ELEMENT METHOD | Gas Turbine Research Establishment, Bengaluru |
| 26 | UR16AE028 | BOMMALI ANUSHA | STRESS ANALYSIS OF AERO ENGINE'S HP COMPRESSOR AND TURBINE'S MAIN SHAFT USING FEM | Gas Turbine Research Establishment, Bengaluru |
| 27 | UR16AE029 | JIM DANIEL | DESIGN AND DEVELOPMENT OF A WEATHER MONITORING NANO DRONE | AFI Technology Aeromodelling and Drones Academy, Coimbatore |
| 28 | UR16AE031 | SINI B DAVID | DESIGN OF RAISED LIP AIR INTAKE FOR COOLING OF AN UAV ENGINE | Aeronautical Development Establishment, Bengaluru |
| 29 | UR16AE035 | RIKTI KIRITKUMAR PRAVASI | COMPARATIVE STUDY BETWEEN DESIGNING AND ANALYSIS OF WEDGE FLOW METER AND VENTURIMETER FOR THE ESTIMATION OF THE MASS FLOW RATE | Defence Research and Development Laboratory, Hyderabad |
| 30 | UR16AE037 | MUHAMMED SHIMNAD | MODELLING OF AIR COOLING SCOOP DUCT FOR AIRCRAFT ENGINE | Aeronautical Development Establishment, Bengaluru |
| 31 | UR16AE038 | ANUSHKA KOSHY | GEOMETRIC GENERATION AND MODELING OF A CIRCULAR TO ELLIPTICAL CURVED ENGINE EXHAUST | Aeronautical Development Establishment, Bengaluru |
| 32 | UR16AE039 | SUDARSHAN K K | CIRCULAR TO ELLIPTICAL VARYING AREA NOZZLE DUCT GEOMETRY GENERATION AND ANALYSIS | Aeronautical Development Establishment, Bengaluru |
| 33 | UR16AE041 | SAM RONALD V | CURRENT PRATICES AND ANALYSIS OF SECTORIAL, CONFIGURATION OF AERO ENGINE MAIN SHAFT | Gas Turbine Research Establishment, Bengaluru |
| 34 | UR16AE042 | DELVIN FELIX D | NON-LINEAR STATIC ANALYSIS OF REAR BUMPER AND NOSE LANDING GEAR WITH IMPACT LOADING AND NORMAL MODES | CADD Centre, Bengaluru |
| 35 | UR16AE043 | DELVIN S SAMUEL | ACCELERATED AGING EXPERIMENTS FOR PROGNOSTICS OF DAMAGE GROWTH IN COMPOSITE MATERIALS | Vikram Sarabhai Space Centre, Thiruvananthapuram |
| 36 | UR16AE048 | JEENA SARA JOHN VARGHESE | COMPARATIVE STUDY BETWEEN THE DESIGN AND ANALYSIS OF DEBIT-METER AND VENTURI-METER WITH DIFFERENT SONIC THROAT CONTOUR DESIGN. | Defence Research and Development Laboratory, Hyderabad |
| 37 | UR16AE053 | SHANKARSHNA S | FLOW ANALYSIS OF VARIOUS PLANES OF HYBRID AIRCRAFT WITH DIFFERENT ANGLE OF ATTACK | Indian Space Research Organisation, Andhra Pradesh |
| 38 | UR16AE058 | GAJALA RAJO BABA FAREED NIYAZI | STRESS ,THERMAL ANALYSIS AND LIFE CALCULATIONS OF HIGH PRESSURE TURBINE AND COMPRESSOR MAIN SHAFT | Gas Turbine Research Establishment, Bengaluru |
| 39 | UR16AE061 | GLORY J | CFD STUDIES ON THE UPSTREAM NOZZLE OF THE PREFILMING AIRBLAST ATOMIZER OF A GAS TURBINE ENGINE COMBUSTOR | Gas Turbine Research Establishment, Bengaluru |
| 40 | UR16AE065 | FRENO FAHAD R | COMPUTATIONAL ANALYSIS OF PRESSURE VARIATION OF SQUEEZE FILM DAMPER IN AERO-GAS TURBINE ENGINE | Gas Turbine Research Establishment, Bengaluru |
| 41 | UR16AE067 | NITESH RAJ | DESIGNING OF A CIRCULAR TO ELLIPTICAL CONSTANT AREA NOZZLE DUCT | Aeronautical Development Establishment, Bengaluru |
| 42 | UT16AE002 | ATHIRA MANIKANDAN | LAMINAR FLOW PREDICTION ON A ROTATING DISC USING BEZIER CURVES | Gas Turbine Research Establishment, Bengaluru |
| 43 | UR16AE044 | RUBAN RJ | NORMAL MODE/MODAL ANALYSIS OF REAR UNDER RUN PROTETION DEVICE (RUPD) | Black Space Research and Development, Karnataka |
| 44 | URK17AE002 | FEBIN P VARGHESE | DESIGN AND ANALYSIS OF ASCENT TRAJECTORY FROM MOON'S SURFACE TO THE MOON'S ORBIT | TeamIndus, Bangalore |
| 45 | URK17AE003 | JOSHUA J | STUDY THE BEHAVIOUR OF MORPHING WING | Black Space Research and Development, Karnataka |
| 46 | URK17AE005 | SAJITH MON S | LINEAR STATIC ANALYSIS OF NESTAINER CONTAINERS | Black Space Research and Development, Karnataka |
| 47 | URK17AE009 | SHERBIN SAM S | STATIC ANALYSIS OF SIDE STEP OF CAR | Black Space Research and Development, Karnataka |
| 48 | URK17AE010 | AVR AKILANDESWARRI | DESIGN OF FRONT SPAR WING-ROOT SEGMENT FOR A SMALL TRANSPORT AIRCRAFT | Bangalore Airctaft Industries Private Limited, Bangalore |
| 49 | URK17AE011 | N.DINESH | LINEAR STATIC ANALYSIS OF REAR UNDERRUN PROTECTION DEVICE | Black Space Research and Development, Karnataka |
| 50 | URK17AE018 | I SOUZAN SUHANA | TO DESIGN AND ANALYZE SUITABLE TRAJECTORIES FROM MOON TO EARTH | TeamIndus, Bangalore |
| 51 | URK17AE023 | ARYA SUBHASH | DESIGN OF A WING-FUSELAGE CONNECTING BRACKET FOR A TRANSPORT AIRFRAME | Bangalore Airctaft Industries Private Limited, Bangalore |
| 52 | URK17AE024 | SAM EMMANUEL ROZARIO | EVALUATION OF SHAPE OF THE CUTOUT FOR THE BOTTOM SKIN IN A TRANSPORT AIRCRAFT WING STRUCTURE | Bangalore Airctaft Industries Private Limited, Bangalore |
| 53 | URK17AE029 | JYOTSANA SUMAN | ELECTRIC PROPULSION IN AIRCRAFT WITH BATTERY ENHANCEMENT TECHNOLOGY USING 3D PRINTING | Black Space Research and Development, Karnataka |
| 54 | URK17AE030 | VENKATESHWARAN | STUDY THE BEHAVIOUR OF BUMPER GRILL BY PERFORMING LINEAR STATIC ANALYSIS | Black Space Research and Development, Karnataka |
| 55 | URK17AE033 | VIVASHVA SUNDAR S | LINEAR STATIC ANALYSIS ON MOTORCYCLE SCISSOR LIFTER | Black Space Research and Development, Karnataka |
| 56 | URK18AE014 | Vinith A | Detection Of Tea Leaf Diseases Using Ai And Uav | Object Automation Software Solution Pvt Ltd, Chennai |
| 57 | URK18AE001 | Suganya | Air Purifying Drone | Jet Aerospace Aviation Research Center, Kerala |
| 58 | URK18AE045 | Deepthi | Forest Fire Detection With Uav | Object Automation Software Solution Pvt Ltd, Chennai |
| 59 | URK18AE023 | Aniket Bhardwaj | Development And Testing Of Umav | IIT Kanpur |
| 60 | URK18AE038 | Sherly Joe S | Estimation Of The Amount Of Propellant Required To Traverse A Given Lunar Trajectory | ISRO Bangalore |
| 61 | URK18AE044 | Jayaraj M | Estimation Of The Amount Of Propellant Required To Traverse A Given Lunar Trajectory | ISRO Bangalore |
| 62 | URK18AE020 | S Sam Kingsley | Estimation Of The Amount Of Propellant Required To Traverse A Given Lunar Trajectory | ISRO Bangalore |
| 63 | URK18AE024 | Sam Sweety Lilly .S | Estimation Of The Amount Of Propellant Required To Traverse A Given Lunar Trajectory | ISRO Bangalore |
| 64 | URK19AE1046 | Joyclyn Priyanka P | Study of The Importance Of Electronic Speed Controller In Drone | Circuitects Electronics Solutions Pvt Ltd., Bangalore |
| 65 | URK19AE1032 | Jerin Suresh | Study of Damage Control On Hybrid Composites | Roquette India Private Limited, Karnataka |
| 66 | URK19AE1024 | Raksha S A | Sandwich Structures For Spacecraft Design | Starops Systems Private Limited, Bengaluru |
| 67 | URK19AE1037 | Sona Sherin.S | Multibody Dynamic Analysis For Unmanned Ground Support Vehicle | Kumaraguru Centre for Industrial Research & Innovation, Coimbatore |
| 68 | URK19AE1026 | Yamuna B M | Design & Analysis of Centrifugal Pump Impeller For Aircraft Liquid Colants | Ametek Instruments India Private Limited, Bangalore |
| 69 | URK19AE1001 | Gummalla Purna Lavanya | Design And Analysis of Bird Detection And Deflection System In Jet Engine | Mech Wind Technologies, Hyderabad |
| 70 | URK19AE1017 | V G Esmitha Ganesan | Numerical Simulation Of Magnetohydrodynamic Flow In An Expansion Duct | Indian Institute of Technology Madras, Chennai |
| 71 | URK19AE1012 | Saravanakumar M | Experimental Evaluation of Dynamic Environment During Launch Vehicle Lift-Off | Satish Dhawan Space Centre - SDSC, Andhra Pradesh |
| 72 | URK19AE1028 | Anakha Manoj | Design of Upper Skin For A Transport Aircraft Wing By Considering Buckling As A Design Driver | Bangalore Aircraft Industries Pvt. Ltd, Bangalore |
| 73 | URK19AE1039 | Priyanshi Paul | Optimal Collisiono Avoidance Maneuvering Strategy: V Directinoal Analaysis For Multigation Of Potential Thrust | ISTRAC ISRO, Bangalore |
| 74 | URK19AE1025 | Karthik Diwakar | Design Optimization of A Star Sensor Mountiing Bracket | U R RAO Satellite Centre, Bangalore |
| 75 | URK19AE1041 | Bijoe Stephen Manjesh | Computational Study To Investigate Cross Flow Effects On Discharge Coefficient | Vikram Sarabhai Space Centre (VSSC), Trivandrum |
| 76 | URK19AE1022 | Joyal Joshi | Computational Study To Investigate The Effects On Cross Flow On Discharge Coefficient At Transonic Regime | Vikram Sarabhai Space Centre (VSSC), Trivandrum |
| 77 | URK19AE1048 | Damuluri Suraj Bharajathya | Altitude Estimation of Space Objects Using Optical Light Curve | ISRO Telemetry Tracking and Command Network (ISTRAC), Bangalore |
| 78 | URK19AE1031 | Simran Gill | Study of Model Reduction Methods In Fea And Its Practical Applications In Spacecraft | Starops Systems Private Limited, Bengaluru |
| 79 | URK19AE1038 | Prem Chandran C | Cfd Analysis On Battery Thermal Managment System | Kumaraguru Centre for Industrial Research & Innovation, Coimbatore |
