Aerodynamics-II detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AE61), 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 6th sem syllabus for be 2017 scheme vtu you can visit Aero 6th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for aerodynamics-ii is as follows.
Course Objectives:
This course will enable students to
- Understand the concepts of compressible flow and shock phenomenon
- Acquire the knowledge of oblique shock and expansion wave formation.
- Appreciate the measurement in high speed flow.
Module 1
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Module 2
Normal Shock: Prandtl Meyer equation and Rankine – Hugonoit relation, Normal shock equations: Property ratios in terms of upstream Mach number, Numericals, Moving Normal Shock wave.
Module 3
Oblique shocks and Expansion waves: Prandtl equation and Rankine – Hugonoit relation, Normal shock equations, Pitot static tube, corrections for subsonic and supersonic flows, Oblique shocks and corresponding equations, Hodograph and pressure turning angle, shock polars, flow past wedges and concave corners, strong, weak and detached shocks, Flow past convex corners, Prandtl -Meyer expansion function, Reflection and interaction of shocks and expansion, waves, Families of shocks. Flow with Friction and Heat transfer.
Module 4
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Module 5
Measurements in High speed Flow: Types of subsonic wind tunnels -Balances and measurements – Interference effects- transonic, Supersonic and hypersonic wind tunnels and characteristic features, their operation and performance – Shock tubes and shock tunnels – Free flight testing -Measurements of pressure, velocity and Mach number -Flow visualization methods of subsonic and supersonic flows.
Course Outcomes:
After studying this course, students will be able to:
- Utilize the concepts of compressible flow and shock phenomenon
- Apply knowledge of oblique shock and expansion wave formation.
- Measure the parameters high speed flow.
Graduate Attributes (as per NBA):
- Engineering Knowledge.
- Problem Analysis.
- Design / development of solutions
- Interpretation of data
Question paper pattern:
- The question paper will have ten questions.
- Each full question consists of 16 marks.
- There will be 2full questions (with a maximum of four sub questions) from each module.
- Each full question will have sub questions covering all the topics under a module.
- The students will have to answer 5 full questions, selecting one full question from each module.
Text Books:
- John D Anderson, Modern Compressible Flow, Mc Graw Hill,3rd edition, 2012, ISBN-13: 978-1259027420.
- Radhakrishnan, E., Gas Dynamics, Prentice Hall of India,5th edition,2014,ISBN-13: 9788120348394
Reference Books:
- Ascher. H. Saphiro, Dynamics and Thermodynamics of Compressible fluid flow, John Wiley & Sons,1st edition,1977, ISBN-13: 978-0471066910.
- Yahya, S.M., Fundamentals of Compressible flow, NEW AGE, 2009, ISBN-13: 9788122426687.
- H.W. Liepmann and A. Roshko, Elements of Gas Dynamics, Dover Publications Inc,2003, ISBN-13: 978-0486419633.
- Hodge B. K, Koenig K, Compressible Fluid Dynamics with Computer Application, 1st edition, Prentice Hall, New York (1995).
- Clancy L. J., Aerodynamics, Shroff Publishers, 2006, ISBN-13: 978-8175980570.
- Zucrow, M.J. and Anderson, J.D., Elements of gas dynamics, McGraw – Hill Book Co., New York, 1989.
For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 6th Sem syllabus for 2017 scheme.
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