The department of Aeronautical Engineering was started in the academic year 2011-12 with an authorized intake of 60 students per annum. At present there are about 240 students, not only from all over India...

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To build outstanding teaching and research environment in the field of Aeronautical Engineering that equips the students with the latest theoretical and practical knowledge and enhances their opportunities in the ..

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Students of the 6th Semester, Niraj Panthi, Ebin Baby, have successfully completed an Innovation and Entrepreneur Development Cell (IEDC), NMIT, sponsored project titled, "Foot Step Energy Harvester"...

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Infrastructure Facilities

The department of Aeronautical Engineering has laboratory and computing facilities. At present, the department has Laboratories for Structures, Propulsion, Modeling and Simulation. The department has a Low Speed Wind Tunnel. The faculty and students work in collaboration with other departments of NMIT. Other facilities include workshops and Laboratories for Energy Conversion , Foundry and Forge, Fluid Mechanics, Measurements and Metrology , Materials Testing. Flight Simulation, Flight Vehicle Design and Unmanned Aerial Vehicle (UAV) Laboratories will be setup at the department soon. A brief description of existing laboratory facilities is given below.

Structures laboratory

A state of the art Structures Laboratory includes test rigs that students use to study the structural analysis and design of an aircraft. NMIT is unique in that it provides these facilities for learning.

Propulsion laboratory

Students and researchers use the propulsion laboratory to conduct experiments related to aircraft engines, force measurements through wall jets and measurement of speed of flame propagation.

Modeling and Simulation Laboratory

The Modeling and Simulation laboratory is equipped with software packages such as ANSYS Workbench, CFD Tools MATLAB and SIMULINK that are to students. Typical ANSYS/CFD analysis results for an airfoil are shown below:

Analysis using ANSYS Workbench  

Zoomed view of the flow domain  
Low Speed Wind Tunnel

The Aerodynamics laboratory is well equipped with a computerized Low Speed Wind Tunnel that is used to demonstrate the nature of flow using flow visualization techniques. The nature of pressure distribution over various body shapes such as symmetrical airfoils, asymmetrical airfoils, and cylinders can be studied. The Wind Tunnel is also fitted with a 3-Component Force Balance that can be used to study the lift, drag and pitching moments on airfoils at different angles of attack and flow velocities.

Low Speed Wind Tunnel  

Test Section and Instruments of Low Speed Wind Tunnel  

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