Aerodynamics Lab Aero 5th Sem Syllabus for VTU BE 2017 Scheme

Aerodynamics Lab detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AEL57), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.

For all other aero 5th sem syllabus for be 2017 scheme vtu you can visit Aero 5th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for aerodynamics lab is as follows.

Course Objectives:

This course will enable students to

1. Be acquainted with basic principles of aerodynamics using wind tunnel.
2. Acquire the knowledge on flow visualization techniques.
3. Understand the procedures used for calculating the lift and drag.
4. Calibration of a subsonic wind tunnel: test section static pressure and total head distributions.
5. Smoke flow visualization studies on a two-dimensional circular cylinder at low speeds.
6. Smoke flow visualization studies on a two dimensional airfoil at different angles of incidence at low speeds
7. Smoke flow visualization studies on a two dimensional multi element airfoil with flaps and slats at different angles of incidence at low speeds
8. Tuft flow visualization on a wing model at different angles of incidence at low speeds: identify zones of attached and separated flows.
9. Surface pressure distributions on a two-dimensional smooth circular cylinder at low speeds and calculation of pressure drag.
10. Surface pressure distributions on a two-dimensional rough circular cylinder at low speeds and calculation of pressure drag.
11. Surface pressure distributions on a two-dimensional symmetric airfoil
12. Surface pressure distributions on a two-dimensional cambered airfoil at different angles of incidence and calculation of lift and pressure drag.
13. Calculation of total drag of a two-dimensional circular cylinder at low speeds using pitot-static probe wake survey.
14. Calculation of total drag of a two-dimensional cambered airfoil at low speeds at incidence using pitot-static probe wake survey.
15. Measurement of a typical boundary layer velocity profile on the tunnel wall (at low speeds) using a pitot probe and calculation of boundary layer displacement and momentum thickness.
16. Calculation of aerodynamic coefficients forces acting on a model aircraft

using force balance at various angles of incidence, speed.

17. Measurement of a typical boundary layer velocity profile on the airfoil at various angles of incidence from leading edge to trailing edge.

Course Outcomes:

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Conduct of Practical Examinations:

1. All lab practicals are to be included for practical examination.
2. Students are allowed to pick one experiment from the lot.
3. Strictly follow the instructions as printed on the cover page of answer script for breakup of marks.
4. Change of experiment is allowed only once and 15% Marks allotted to the procedure part to be made zero.

Graduate Attributes (as per NBA):

• Engineering Knowledge.
• Problem Analysis.
• Design / development of solutions (partly)
• Interpretation of data.

For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 5th Sem syllabus for 2017 scheme.

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