School of Mechanical & Manufacturing Engineering
Department: Department of Aerospace Engineering Teaching Lab Facilities

Teaching Lab Facilities

1- AERODYNAMICS 

Facilities Available
  • Air Bench Apparatus
  • Axial Fan Flow Apparatus
  • Flight Demonstration Wind Tunnel
  • Free and Forced Vortex Apparatus
  • Osborne Reynold Equipment
  • Animal house
  • Smoke Tunnel
  • Hydraulic Bench

2- AEROSTRUCTURES 

Facilities Available
  • UTM 100kN with DAQ System
  • Impact Testing Machine
  • Creep Testing Machine
  • Shearing Force Apparatus and Bending Moment Apparatus
  • Torsion Testing Machine 300Nm and 50Nm
  • Strain Gauge Apparatus with Bending, Torsion and Tensile Testing samples
  • Column Buckling Apparatus
  • Unsymmetrical Cantilever Apparatus
  • Fatigues Testing Machine
  • Universal Hardness Tester

3 – Aerodynamics  

Facilities Available
  • Test Section Dimensions: 18” × 18” × 36” Open Circuit Tunnel
  • Airspeed Range: 2-60 m/s
  • Turbulence Intensity Level: 0.1-0.25%
  • Honeycomb Flow Straightener
  • Turbulence-reducing Screens: Four (4) 0.1% of turbulence level
  • Contraction Ratio: 9:1
  • Approx. Tunnel Dimension (Length x Width x Height): 30” × 05” × 07”

4 – Thermodynamics  

Facilities Available
  • Temperature Measurement Bench
  • Pressure Measurement Bench
  • Marcet Boiler
  • Oxygen Bomb Calorimeter
  • Mechanical Heat Pump Apparatus
  • Steam Power Plant with Steam Engine
  • Single Stage Air Compressor Apparatus
  • Spark Ignition Engine, 4 Cylinder in line, 4-strokes Cut Model
  • Spark Ignition Engine, Single Cylinder Engine Cut Model

5 – Heat and Mass Transfer  

Facilities Available
  • Heat Conduction Study Unit (Linear, Radial)
  • Free & Forced Convection Heat Transfer
  • Radiation Heat Transfer Apparatus
  • Thermal Conductivity of Liquid & Gases Apparatus
  • Multi Heat Exchanger Service Unit
  • Concentric Tube Heat Exchanger
  • Shell & Tube Type Heat Exchanger

6 – Electrical & Electronics  

Facilities Available
  • DC Power Supply
  • Function Generators (10MHz)
  • Breadboards
  • Benchtop Multimeters
  • LCR Meters
  • Programmable Power Supply
  • Logic Probes

7 – Computer Lab  

Facilities Available
  • Dell Core i7 13 Gen
  • 32 GB RAM
  • 512 GB SSD
  • 1 TB HDD
  • Mouse, Keyboard
  • Windows 11 Pro
  • 24” LCD

8 – Propulsion  

Facilities Available
  • F7P Aircraft WP-7B Engine
  • Combustion Laboratory Unit Dual Fuel Type with DAQ
  • Gas Turbine Jet Engine 100N Thrust with DAQ Model
  • Nozzle Performance Apparatus with Nozzles Qty: 5 and Air Compressor
  • Computer Controlled Axial Flow Gas Turbine Engine Model: TGFAC
  • Nozzle Pressure Distribution Apparatus (TH-3197)
  • Air Operated Impulse Turbine
  • Solar Photovoltaic System
  • Water Cooling Tower (Model: TH 3130)
  • Francis Turbine Test Rig (FM-1849-15R)
  • Wind Turbine AC/DC Module
  • Jet Engine & Aircraft Instruments (Altimeter, Air Speed Indicator, Climb and Dive Indicator, Turn and Slip Indicator, Compass Indicator, Vertical and Velocity Indicator, Fuel Indicator, Mach Meter)

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