AE3401 Syllabus - Aerodynamics I - 2021 Regulation Anna University
AE3401 Syllabus - Aerodynamics I - 2021 Regulation Anna University
AE3401 | AERODYNAMICS I | LTPC |
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3003
COURSE OBJECTIVES:
• To introduce the concepts of mass, momentum and energy conservation
relating to aerodynamics.
• To introduce the Navier Stroke equations and its application
• To make the student understand the concept of vorticity, irrotationality, theory of airfoil and wing sections.
• To introduce the basics of viscous flow.
• To make the student to understand the different boundary layers and Blasius Solution
• To introduce the basics of turbulence flow
• To introduce the Navier Stroke equations and its application
• To make the student understand the concept of vorticity, irrotationality, theory of airfoil and wing sections.
• To introduce the basics of viscous flow.
• To make the student to understand the different boundary layers and Blasius Solution
• To introduce the basics of turbulence flow
UNIT I | INTRODUCTION TO LOW-SPEED FLOW | 9 |
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Euler equation, incompressible Bernoulli’s equation. circulation and
vorticity, green’s lemma and Stoke’s theorem, barotropic flow, kelvin’s
theorem, streamline, stream function, irrotational flow, potential
function, Equipotential lines, elementary flows and their combinations.
UNIT II | TWO-DIMENSIONAL INVISCID INCOMPRESSIBLE FLOW | 9 |
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Ideal Flow over a circular cylinder, D’Alembert’s paradox, magnus effect,
Kutta Joukowski’s theorem, starting vortex, Kutta condition, real flow
over smooth and rough cylinder.
UNIT III | AIRFOIL THEORY | 9 |
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Cauchy-Riemann relations, complex potential, methodology of conformal
transformation, Kutta- Joukowski transformation and its applications, thin
airfoil theory and its applications.
UNIT IV | SUBSONIC WING THEORY | 9 |
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Vortex filament, Biot and Savart law, bound vortex and trailing vortex,
horse shoe vortex, lifting line theory and its limitations.
UNIT V | INTRODUCTION TO BOUNDARY LAYER THEORY | 9 |
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Boundary layer and boundary layer thickness, displacement thickness,
momentum thickness, energy thickness, shape parameter, boundary layer
equations for a steady, two-dimensional incompressible flow, boundary
layer growth over a flat plate, critical Reynolds number, Blasius
solution, basics of turbulent flow.
TOTAL: 45 PERIODS
COURSE OUTCOMES: On completion of the course, the student is expected
to be able to
CO1: Apply the basics physics for low-speed flows.
CO2: Apply the concept of 2D, inviscid incompressible flows in low-speed aerodynamics.
CO3: Solve lift generation problems using aerofoil theories.
CO4: Make use of lifting line theory for solving flow properties.
CO5: Solve the boundary layer equations for a steady, two-dimensional incompressible flow
CO6: Solve the properties of turbulent flow.
CO2: Apply the concept of 2D, inviscid incompressible flows in low-speed aerodynamics.
CO3: Solve lift generation problems using aerofoil theories.
CO4: Make use of lifting line theory for solving flow properties.
CO5: Solve the boundary layer equations for a steady, two-dimensional incompressible flow
CO6: Solve the properties of turbulent flow.
TEXT BOOKS:
1. Anderson, J.D., "Fundamentals of Aerodynamics", McGraw Hill Book Co.,
2010
2. Houghton, E.L., and Caruthers, N.B., "Aerodynamics for Engineering students", Edward Arnold Publishers Ltd., London, 1989.
3. E Rathakrishnan, “Theoretical Aerodynamics”, John Wiley, NJ, 2013
2. Houghton, E.L., and Caruthers, N.B., "Aerodynamics for Engineering students", Edward Arnold Publishers Ltd., London, 1989.
3. E Rathakrishnan, “Theoretical Aerodynamics”, John Wiley, NJ, 2013
REFERENCES:
1. Clancey, L J.," Aerodynamics", Pitman, 1986
2. John J Bertin., "Aerodynamics for Engineers", Pearson Education Inc, 2002
3. Kuethe, A.M and Chow, C.Y, “Foundations of Aerodynamics”, Fifth Edition, John Wiley & Sons, 2000.
4. Milne Thomson, L.H., "Theoretical Aerodynamics", Macmillan, 1985
2. John J Bertin., "Aerodynamics for Engineers", Pearson Education Inc, 2002
3. Kuethe, A.M and Chow, C.Y, “Foundations of Aerodynamics”, Fifth Edition, John Wiley & Sons, 2000.
4. Milne Thomson, L.H., "Theoretical Aerodynamics", Macmillan, 1985
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