VTU B.TECH Aeronautical-Engineering 2nd year SEMESTER – VII Syllabus For Fundamentals of aerodynamic theory PDF 2022
February 12, 2022 2022-02-12 23:22VTU B.TECH Aeronautical-Engineering 2nd year SEMESTER – VII Syllabus For Fundamentals of aerodynamic theory PDF 2022
VTU B.TECH Aeronautical-Engineering 2nd year SEMESTER – VII Syllabus For Fundamentals of aerodynamic theory PDF 2022
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You will be able to find information about Fundamentals of aerodynamic theory 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 Fundamentals of aerodynamic theory after reading this blog. Fundamentals of aerodynamic theory has 5 units altogether and you will be able to find notes for every unit on the CynoHub app. Fundamentals of aerodynamic theory 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.
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Fundamentals of aerodynamic theory Unit One
Review of Basic Fluid Mechanics
Continuity, momentum and energy equation, Control volume approach to Continuity, momentum and energy equation, Types of flow, pathlines, streamlines, and streaklines, units and dimensions, inviscid and viscous flows, compressibility, Mach number regimes. Vorticity, Angular velocity, Stream function, velocity potential function, Circulation, Numericals, Mach cone and Mach angle, Speed of sound.
Fundamentals of aerodynamic theory Unit Two
Airfoil Characteristics
Fundamental aerodynamic variables, Airfoil nomenclature, airfoil characteristics. wing planform geometry, aerodynamic forces and moments, centre of pressure, pressure coefficient, aerodynamic center, calculation of airfoil lift and drag from measured surface pressure distributions, typical airfoil aerodynamic characteristics at low speeds. Types of drag-Definitions.
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Fundamentals of aerodynamic theory Unit Three
Module-3
Two Dimensional Flows & Incompressible Flow Over Airfoil Uniform flow, Source flow, Sink flow, Combination of a uniform flow with source and sink. Doublet flow. Non-lifting flow over a circular cylinder. Vortex flow. Lifting flow over a circular cylinder. Kutta-Joukowski theorem and generation of Lift, D’Alembert’s paradox, Numericals, Incompressible flow over airfoils: Kelvin’s circulation theorem and the starting vortex, vortex sheet, Kutta condition, Classical thin airfoil theory for symmetric and cambered airfoils. Kutta-Joukowski theorem and generation of Lift, Numericals.
Fundamentals of aerodynamic theory Unit Four
Incompressible Flow Over Finite Wings
Biot-Savart law and Helmholtz’s theorems, Vortex filament: Infinite and semi-infinite vortex filament,Induced velocity. Prandtl’s classical lifting line theory: Downwash and induced drag. Elliptical and modified elliptical lift distribution. Lift distribution on wings. Limitations of Prandtl’s lifting line theory. Extended lifting line theory- lifting surface theory, vortex lattice method for wings. Lift, drag and moment characteristics of complete airplane.
Fundamentals of aerodynamic theory Unit Five
Applications of Finite Wing Theory & High Lift Systems
Simplified horse-shoe vortex model, formation flight, influence of downwash on tail plane, ground effects. Swept wings: Introduction to sweep effects, swept wings, pressure coefficient, typical aerodynamic characteristics, Subsonic and Supersonic leading edges. Introduction to high-lift systems, flaps, leading-edge slats and typical high – lift characteristics. critical Mach numbers, Lift and drag divergence, shock induced separation, Effects of thickness, camber and aspect ratio of wings, Transonic area rule, Tip effects. Introduction to Source panel & vortex lattice method.
Fundamentals of aerodynamic theory Course Objectives
Understand the basics of fluid mechanics as a prerequisite to Aerodynamics •Acquire knowledge on typical airfoil characteristics and two-dimensional flows over airfoil and study the incompressible over finite wings •Assimilate the understanding of application of finite wing theory and high lift systems
Fundamentals of aerodynamic theory Course Outcomes
At the end of the course the student will be able to:1.CO1 :Evaluate typical airfoil characteristics and two-dimensional flows over airfoil 2.CO2 :Compute and analyse the incompressible flow over finite wings
CO3 : Apply finite wing theory and design high lift systems from the aerodynamics view point Question paper pattern:
Fundamentals of aerodynamic theory Text Books
Fundamental of Aerodynamics-Anderson
J.D
Aerodynamics for Engineering Students-E. L. Houghton, P.W. Carpenter
Fundamentals of aerodynamic theory Reference Books
Aerodynamics-Clancy L. J.
Theoretical Aerodynamics-Louis M. Milne-Thomson
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