Aerodynamics-II detailed Syllabus for Aerospace Engineering (AS), 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 AS 5th Sem Syllabus for BE 2018 Scheme, do visit VTU AS 5th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for aerodynamics-ii is as follows.
Course Objectives:
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Module 1
One Dimensional Compressible Flow: Energy, Momentum, continuity and state equations, velocity of sound, Adiabatic steady state flow equations, Flow through converging, diverging passages, Performance under various back pressures. Numericals.
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
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Module 4
Differential Equations of Motion for Steady Compressible Flows: Basic potential equations for compressible flow. Linearisation of potential equation-small perturbation theory. Methods for solution of nonlinear potential equation -Introduction, Method of characteristics, Boundary conditions, Pressure coefficient expression, small perturbation equation for compressible flow-Prandtl, Glauret and Geothert’s rules-Ackert’s supersonic airfoil theory, Von-Karman rule for transonic flow, Lift, drag pitching moment and center of pressure of supersonic profiles.
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:
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Question paper pattern:
- The question paper will have ten full questions carrying equal marks.
- Each full question will be for 20 marks.
- There will be two full questions (with a maximum of four sub- questions) from each module.
- Each full question will have sub- question covering all the topics under a module.
- The students will have to answer five full questions, selecting one full question from each module.
Text Books:
- Modern Compressible Flow John D Anderson Mc Graw Hill 3rd edition, 2012
- Gas Dynamics Radhakrishnan, E Prentice Hall of India 5 th edition,2014
Reference Books:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
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For detail Syllabus of all other subjects of BE 5th Sem Aerospace Engineering, visit (AS) 5th Sem Syllabus Subjects.
For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.