Aerodynamics II detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8503), Category (PC), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.
For all other aero 5th sem syllabus for be 2017 regulation anna univ you can visit Aero 5th Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for aerodynamics ii is as follows.”
Course Objective:
- To introduce the concepts of compressibility,
- To make the student understand the theory behind the formation of shocks and expansion fans in Supersonic flows.
- To introduce the methodology of measurements in Supersonic flows.
Unit I
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Unit II
Normal and Oblique Shocks
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 polar, flow past wedges and concave corners, strong, weak and detached shocks,
Unit III
Expansion Waves and Method of Characteristics
Flow past convex corners, Expansion hodograph, Reflection and interaction of shocks and expansion, waves. Method of Characteristics Two dimensional supersonic nozzle contours. Rayleigh and Fanno Flows.
Unit IV
For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.
Unit V
Transonic Flow Over Wing
Lower and upper critical Mach numbers, Lift and drag, divergence, shock induced separation, Characteristics of swept wings, Effects of thickness, camber and aspect ratio of wings, Transonic area rule. Introduction to Hypersonic Aerodynamics.
Course Outcome:
- Calculate the compressible flow through a duct of varying cross section.
- Use quasi one-dimensional theory to analyze compressible flow problems.
- Estimate fluid properties in Rayleigh and Fanno type flows.
- Estimate the properties across normal and oblique shock waves.
- Predict the properties of hypersonic flows.
Text Books:
- Anderson Jr., D., – Modern compressible flows, McGraw-Hill Book Co., New York, 1999.
- L.J. Clancy, Aerodynamics Sterling Book House, 2006
References:
- Rathakrishnan, E., Gas Dynamics, 6th Edition, Prentice Hall of India, 2017.
- Shapiro, A.H., Dynamics and Thermodynamics of Compressible Fluid Flow, Ronald Press, 1982.
- 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 regulation do visit Aero 5th Sem syllabus for 2017 Regulation.
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