Infrastucture/Facilities

Department of Aeronautical Engineering has the best infrastructure and state – of – the – art modern high tech laboratory facilities such as; Fluid Mechanics laboratory, Aircraft structures Laboratory, Propulsion Laboratory, Energy Conversion Laboratory, Aerodynamics Laboratory, Aircraft Simulation Laboratory and Design, Modelling and Analysis Laboratory. Details of the list of equipments available in each laboratories are listed here.


Laboratory details with major equipments.
Sl. No. Laboratory Description
1 STRUCTURES LAB Wagner  beam set-upBeam test set-up
Vibration set-up with vibration set-up accelerator  meter with computer
Furniture and other equipments>
2 AIRCRAFT PROPULSION LAB.

Forced Convection Apparatus,
Study of performance  of a propeller set-up,
Measurement of Nozzle flow equipment,
Cascade testing of model axial flow compressor blade row,
Measurement of burning velocity flame with compressor,
Bomb calorimeter with oxygen cylinder,
Cascade testing model flow compressor,
Free wall jet  set-up,
Micro Gas Turbine Engine Set-up,
(Furniture and other equipments

3 AERODYNAMICS LAB

Wind tunnel
Smoke generator
Traverse mechanism
Electronic digital manometer,
Wake rake & Boundary layer rake
Furniture and other equipments
Test models

4 ENERGY CONVERSION LAB

Abel flash point apparatus,
Pensky Martin fire point apparatus,
Red wood viscometer,
Say bolt viscometer,
Torsion viscometer,
Boys gas calorimeter,
Valve timing diagram of 4 Stroke diesel engine,
Port diagram for 2 stroke petrol engine,
MPFI  petrol engine cut section,
Mechanical type planimeter,
Digital type Planimeter,
Kirloskar  4 stroke single cylinder diesel engine Test rig water cooled,
Bajaj 2 stroke, air cooled, single cylinder Petrol engine with Hero-Honda Carburetor and alternator,
Single cylinder 4 stroke variable compression ratio (VCR) petrol engine test rig, Morse test set-up greaves
Furniture and other equipments

 5 COMPUTER BASED LAB

HCL Desktop Computers (i3, 6GB RAM, 64 bit operating system),
HP Desktop Computers(i5, 8GB RAM, 64 bit operating system),
Licensed  Software: ANSYS V14,
NASTRAN/PATRAN, CATIA V6, MATLAB 2012a

 6 FLUID MECHANICS LAB

 

Verification of Bernoulli’s theorem- Pressure measurement with Pitot-Static tube.
Performance test on air blower.
Determination of coefficient of friction of flow in pipes.
Determination of minor losses in flow through pipes.
Determination of force developed by impact of jets on vanes.
Determination of Coefficient of discharge for a small orifice by a variable head method. &
Determination of Coefficient of discharge for V-Notch by a variable head method.
Determination of Coefficient of discharge for V- Notches & Weirs by a variable head method.
Performance test of a two stage Reciprocating Air Compressor.
Reynolds apparatus.
Study of Potential flows.
Measurement of force and centre of pressure on a plane surface.

 

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Contact Info

  • Dayananda Sagar College of Engineering, Shavige Malleshwara Hills, Kumarswamy Layout, Bangalore - 78

  • +91-80-42161750+91-80-42161751
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