AE21002: Low Speed Aerodynamics

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AE21002
Course name Low Speed Aerodynamics
Offered by Aerospace Engineering
Credits 4
L-T-P 3-1-0
Previous Year Grade Distribution
4
7
10
15
4
7
3
EX A B C D P F
Semester Spring


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE21001 3 - 1 - 0: 4 CreditsAerofoil characteristics, Classical aerofoil theory â camber and thickness problems, The source and vortex panel numerical methods, Prandtl s lifting line theory, Lifting surface theory, The vortex lattice method and general 3-D panel method, Boundary layer characteristics. Books:E L Houghton and A E Brock, Aerodynamics for Engineering Students, Edward ArnoldE L Houghton and N B Carruthers, Aerodynamics for Engineering Students, Edward ArnoldJ Katz and A E Plotkin, Low Speed Aerodynamics, Cambridge University PressJ D Anderson, Jr., Fundamentals of Aerodynamics, McGraw-Hill InternationalH Schlichting, Boundary Layer Theory, McGraw-Hill


Concepts taught in class[edit | edit source]

Concepts related to potential flow theory before mid-sems and viscous flow theory and related boundary layer theory post midsem


Student Opinion[edit | edit source]

Get a clear idea about basic in-compressible aerodynamics paving the way for further studies

How to Crack the Paper[edit | edit source]

Class notes are very important. Previous years' papers give a good idea about the format of the question paper.

Classroom resources[edit | edit source]

J D Anderson, Jr., Fundamentals of Aerodynamics


Additional Resources[edit | edit source]