4th Sem, AERO

Aerodynamics I Aero 4th Sem Syllabus for BE 2017 Regulation Anna Univ

Aerodynamics I detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8401), Category (PC), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.

For all other aero 4th sem syllabus for be 2017 regulation anna univ you can visit Aero 4th Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for aerodynamics i is as follows.”

Course Objective:

  • To introduce the concepts of mass, momentum and energy conservation relating to aerodynamics.
  • To make the student understand the concept of vorticity, irrotationality, theory of airfoils and wing sections.
  • To introduce the basics of viscous flow.

Unit I

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit II

Two Dimensional Inviscid Incompressible Flow
Ideal Flow over a circular cylinder, DAlemberts paradox, magnus effect, Kutta joukowskis theorem, starting vortex, kutta condition, real flow over smooth and rough cylinder.

Unit III

Airfoil Theory
Cauchy-riemann relations, complex potential, methodology of conformal transformation, kutta-joukowski transformation and its applications, thin airfoil theory and its applications.

Unit IV

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit V

Introduction To Boundary Layer Theory
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.

Course Outcome:

  • An ability to apply airfoil theory to predict airfoil performance
  • Analyze and optimize wing performance
  • A knowledge of incompressible flow
  • A knowledge of subsonic wing theory
  • Apply propeller theory to predict blade performance
  • An exposure to Boundary layer theory

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.

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 and Sons, 2000.
  4. Milne Thomson, L.H., “Theoretical Aerodynamics”, Macmillan, 1985

For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 4th Sem syllabus for 2017 Regulation.

Dont forget to download iStudy for latest syllabus and results, class timetable and more.

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