Aerospace-Engineering

National Aerospace Conceptual Design Competition (NACDeC VI) 2023 – Winners. Department of Aerospace Engineering organizing Skill Development Workshops for Aerospace Students. M.Tech. in Industrial Systems Engineering (Specialization: Model Based Systems Engineering) Consolation prize for Mr. Jayesh Sharma, in SYRES 2023 in PG Category organized by IEEE Hyderabad. Best paper award for Ms. Rinisha T. Nikhade & Dr. Ganapati N. Joshi, International conference STAAAR 2023. SPANDAN 2024 – Department of Aerospace Engineering students won the Institute Rolling Trophy. Patent Successfully granted to Dr. Manish Tripathi, Dr. Ajay Misra, Dr. Mahesh M. S. Consolation prize for Mr. Jayesh Sharma, in SYRES 2023 in PG Category organized by IEEE Hyderabad. Best Paper Award for Jagdish J S, Oshmita A & Dr. Pooja Agrawal, International Conference on Innovations in Infrastructure (ICIlIF 2024), organized jointly by the Institute of Technology Research and Management (TRAM), India, and Université Polytechnique Hauts-de-France (UPHE), France, 2024. Best Paper Award for Srinivasan R, Dr. Sunita Dhavale & Dr. Pooja Agrawal, IEEE International Conference on Robotics and Mechatronics (ICRM), 2025. Best Paper Award for Prajakta Koratkar & Dr. Pooja Agrawal, International Conference on Smart Mechanical Systems for Sustainability (ICSMSS 2025), organized by the Department of Mechanical Engineering, jointly with Indian Society of Manufacturing Engineers, 2025. Best Paper Award for Rahul Chaudhary & Dr. Pooja Agrawal, International Conference on Recent Developments in Control, Automation and Power Engineering (RDCAPE), 2025. Conducted Rubber powered & E20 battery powered airplane building & flying workshop on 13 Jan 2025. Conducted customized course on Missile Technology for BDL Executives from 05 May 2025 to 13 June 2025 Conducted orientation Workshop on Missiles & UAVs on 13-14 Aug 2025 Best Paper Award for Mittapalyam Ashok Karthik, Dr. Ajay Misra & Dr. Ganapati N. Joshi, International Conference on Sustainable Air and Space Technologies (ICSAST – 2025), KITS, 2025
DIAT

Department of Aerospace Engineering and Autonomous Systems

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Aerodynamics Laboratory

Subsonic Wind Tunnel Facility

Test section: 0.6m x 0.6m x 2m;
Max Speed: 30m/s
Instruments: PIV, Hot-wire Anemometer, Pressure Scanner, F/T Sensor, Pressure probes, Micromanometers, Smoke generator

Shock Tube

  • Driver Tube Length: 0.4m

  • Internal Diameter: 0.029m

  • Driven Tube Length: 0.6m

  • Diaphragm material: Tracing paper (90-95 gsm) Diaphragm

    • Table top Hypersonic Shock Tunnel Facility

    Test section: 0.17m x 0.17m x 0.2m;
    Mach No.: 6
    Instruments:

    • Schlieren,
    • Shadowgraph,
    • High Speed Camera,
    • Pressure transducer,
    • Accelerometer,
    • Digital Oscilloscope.

    Computational Facility​

    Work Station
    Software:
  • Starccm+,
  • CFD++,
  • Solidworks,
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