Blog

VTU B.TECH Aeronautical-Engineering 2nd year SEMESTER – V Syllabus For Aerodynamics – ii PDF 2022

Uncategorized

VTU B.TECH Aeronautical-Engineering 2nd year SEMESTER – V Syllabus For Aerodynamics – ii PDF 2022

Spread the love

Get Complete Lecture Notes for Aerodynamics – ii on Cynohub APP

Download the APP Now! ( Click Here )

You will be able to find information about Aerodynamics – ii along with its Course Objectives and Course outcomes and also a list of textbook and reference books in this blog.You will get to learn a lot of new stuff and resolve a lot of questions you may have regarding Aerodynamics – ii after reading this blog. Aerodynamics – ii has 5 units altogether and you will be able to find notes for every unit on the CynoHub app. Aerodynamics – ii can be learnt easily as long as you have a well planned study schedule and practice all the previous question papers, which are also available on the CynoHub app.

All of the Topic and subtopics related to Aerodynamics – ii are mentioned below in detail. If you are having a hard time understanding Aerodynamics – ii or any other Engineering Subject of any semester or year then please watch the video lectures on the official CynoHub app as it has detailed explanations of each and every topic making your engineering experience easy and fun.

Aerodynamics – ii Unit One

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.

Aerodynamics – ii Unit Two

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.

Get Complete Lecture Notes for Aerodynamics – ii on Cynohub APP

Download the APP Now! ( Click Here )

Aerodynamics – ii Unit Three

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. Basics of Fanno and Rayleigh Flow.

Aerodynamics – ii Unit Four

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.

Aerodynamics – ii Unit Five

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.

Aerodynamics – ii Course Objectives

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.

Aerodynamics – ii Course Outcomes

At the end of the course the student will be able to:1.CO1: Utilize the concepts of compressible flow and shock phenomenon 2.CO2: Apply knowledge of oblique shock and expansion wave formation. 3.CO3: Measure the parameters high speed flow.

Aerodynamics – ii Text Books

Modern Compressible Flow-John D
Anderson
Gas Dynamics-Radhakrishnan,E

Aerodynamics – ii Reference Books

Dynamics and Thermodynamics of Compressible fluid flow-Ascher. H. Saphiro
Fundamentals of Compressible flow-Yahya,
S.M
Elements of Gas Dynamics-H.W.
Liepmann and A. Roshko
Compressible Fluid Dynamics with Computer Application-Hodge B. K, Koenig K
Elements of gas dynamics- Zucrow, M.J. and Anderson, J.D

Scoring Marks in Aerodynamics – ii

Scoring a really good grade in Aerodynamics – ii is a difficult task indeed and CynoHub is here to help!. Please watch the video below and find out how to get 1st rank in your B.tech examinations . This video will also inform students on how to score high grades in Aerodynamics – ii . There are a lot of reasons for getting a bad score in your Aerodynamics – ii exam and this video will help you rectify your mistakes and help you improve your grades.

Information about VTU B.Tech Aerodynamics – ii was provided in detail in this article. To know more about the syllabus of other Engineering Subjects of JNTUH check out the official CynoHub application. Click below to download the CynoHub application.

Get Complete Lecture Notes for Aerodynamics – ii on Cynohub APP

Download the APP Now! ( Click Here )

Leave your thought here

Your email address will not be published. Required fields are marked *