Aerodynamics Lab detailed Syllabus for Aeronautical Engineering (AERO), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.
For all other VTU AERO 5th Sem Syllabus for BE 2018 Scheme, do visit VTU AERO 5th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for aerodynamics lab is as follows.
Course Objectives:
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List of Experiments:
- Calibration of a subsonic wind tunnel: test section static pressure and total head distributions.
- Smoke flow visualization studies on a two-dimensional circular cylinder at low speeds.
- Smoke flow visualization studies on a two dimensional airfoil at different angles of incidence at low speeds
- Smoke flow visualization studies on a two dimensional multi element airfoil with flaps and slats at different angles of incidence at low speeds
- Tuft flow visualization on a wing model at different angles of incidence at low speeds: identify zones of attached and separated flows.
- Surface pressure distributions on a two-dimensional smooth circular cylinder at low speeds and calculation of pressure drag.
- Surface pressure distributions on a two-dimensional rough circular cylinder at low speeds and calculation of pressure drag.
- Surface pressure distributions on a two-dimensional symmetric airfoil and estimation of center of
- Surface pressure distributions on a two-dimensional cambered airfoil at different angles of incidence,
- Calculation of total drag of a two-dimensional circular cylinder at low speeds using pitot-static probe wake survey.
- Calculation of total drag of a two-dimensional cambered airfoil at low speeds at incidence using pitot-static probe wake survey.
- 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.
- Calculation of aerodynamic coefficients and forces acting on a model aircraft at various Angle of Attack and speeds using wind tunnel balance (With and Without Yaw).
- Pressure measurements on aerofoil for a case of reverse flow.
Course Outcomes:
At the end of the course the student will be able to:
- Apply the flow visualization techniques.
- Estimate the pressure distribution over the bodies.
- Calculate the lift and drag.
Conduct of Practical Examinations:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
For detail Syllabus of all other subjects of BE 5th Sem Aeronautical Engineering, visit (AERO) 5th Sem Syllabus Subjects.
For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.