The Department of Aeronautical and Automobilecorelab
AERODYNAMICS & PROPULSION LAB
AAE 2241
Syllabus
- 01Introduction to Wind tunnel and Propulsion labs and familiarizing the apparatus
- 02Introduction to wind tunnel and its calibration
- 03flow over a cylinder
- 04Pressure distribution and flow over symmetric and cambered airfoils
- 05Boundary layer calculations
- 06Calculation of zero lift angle and hot wire anemometer
- 07Calculation of drag of a cylinder and airfoil by using wake survey method
- 08Demonstration of 6 component balance and water tunnel visualization
- 09Performance of mini gas turbine
- 10Axial flow fan performance
- 11Free jet and wall jet experiment
- 12Calculation of burning velocity, forced & natural convection
- 13Performance of convergent nozzle
- 14Bomb calorimeter
- 15propeller test rig experiment
References
- Jewel B Barlow, William H Rae, Alan Pope Low speed wind tunnel testing, Wiley-Interscience, (1999)
- J.D. Anderson, Fundamental of Aerodynamics, McGraw-Hill Education; (2016)
- George P. Sutton, Rocket Propulsion Elements, Wiley India Pvt Ltd, (2010)
- National Aeronautics and Space Administration. 1985. Aeronautical Facilities Catalogue. 1: Wind Tunnels (NASA RP-1132). Washington, D.C. National Academies of Sciences, Engineering, and Medicine. 1992. Aeronautical Technologies for the Twenty-First Century. Washington, DC:The National Academies Press. https://doi.org/10.17226/2035
Credits Structure
0Lecture
0Tutorial
3Practical
1Total