Regulation 2021, Anna University Subject code – AE3502 deals with B.E Aeronautical Engineering 3rd year semester V Aerodynamics II Syllabus. To prepare for challenging subjects in the field of Aeronautics need a detailed syllabus and preparation strategies. In this article, we discuss the Aerodynamics II syllabus.
We intend to provide every topic of the syllabus and content required for academic performance, along with reference books. In this article, AE3502 – Aerodynamics II Syllabus, you will be guided to get an idea of each topic of the syllabus and you can make your preparation strategy, and notes by filtering difficult topics from the different subjects. Then you can concentrate on the topic where you need to focus more. We included all the topics regarding the Aeronautical syllabus. We hope this information is useful to you. Don’t forget to share it with your friends and classmates.
If you want to know more about the syllabus of B.E Computer Science and Engineering connected to an affiliated institution’s under four-year undergraduate degree programme. We provide you with a detailed Year-wise, semester-wise, and Subject-wise syllabus in the following link B.E Aeronautical Engineering Syllabus Anna University, Regulation 2021.
Aim Of Concept:
- To introduce the concepts of compressibility,
- To learn the theory behind the formation of shocks and expansion fans in Supersonic flows.
- To introduce the methodology of measurements in Supersonic flows.
- To get knowledge on high-speed flow over airfoils, wings and airplane configuration.
- To learn the concepts of Transonic flow
AE3502- Aerodynamics II Syllabus
Unit I: One-Dimensional Compressible Flow
Energy, Momentum, continuity and state equations, velocity of sound, adiabatic steady-state flow equations, Flow through convergent-divergent passage, Performance under various back pressures.
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: Differential Equations Of Motion For Steady Compressible Flows
Small perturbation potential theory, solutions for supersonic flows, Mach waves and Mach angles, Prandtl-Glauert rule – affine transformation relations for subsonic flows, linearized two-dimensional supersonic flow theory – Lift, drag, pitching moment and center of pressure of supersonic profiles.
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.
Text Books:
1. Anderson Jr., D., – “Modern compressible flows”, McGraw-Hill Book Co., New York, 1999.
2. L.J. Clancy, “Aerodynamics” Sterling Book House, 2006
References:
1. Rathakrishnan, E., “Gas Dynamics”, 6th Edition, Prentice Hall of India, 2017.
2. Shapiro, A.H., “Dynamics and Thermodynamics of Compressible Fluid Flow”, Ronald Press, 1982.
Related Posts On Semester- V: