Aerodynamics II detailed syllabus for Aeronautical Engineering (Aero) for 2021 regulation curriculum has been taken from the Anna University official website and presented for the Aero students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below.
For Aeronautical Engineering 5th Sem scheme and its subjects, do visit Aero 5th Sem 2021 regulation scheme. The detailed syllabus of aerodynamics ii is as follows.
Course Objectives:
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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
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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.
Course Outcomes:
Upon completion of the course, Students will be able to
- Calculate the compressible flow through a duct of varying cross section.
- Use quasi one-dimensional theory to analyse compressible flow problems.
- Estimate fluid properties in Rayleigh and Fanno type flows.
- Estimate the properties across normal and oblique shock waves.
- Understand the knowledge of various techniques and methods for solving differential equations of motion for steady compressible flows.
- Predict the properties of transonic flows.
Text Books:
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Reference Books:
- Rathakrishnan, E., “Gas Dynamics”, 6th Edition, Prentice Hall of India, 2017.
- Shapiro, A.H., “Dynamics and Thermodynamics of Compressible Fluid Flow”, Ronald Press, 1982.
For detailed syllabus of all other subjects of Aeronautical Engineering, 2021 regulation curriculum do visit Aero 5th Sem subject syllabuses for 2021 regulation.
For all Aeronautical Engineering results, visit Anna University Aero all semester results direct link.