Aerospace-Engineering

National Aerospace Conceptual Design Competition (NACDeC vi) 2023 – Winners.         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.        Department of Aerospace Engineering organizing Skill Development Workshops for Aerospace Students.
DIAT

Department of Aerospace Engineering

Defence Institute of Advanced Technology Pune
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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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