AE31009: Aerospace Structural Analysis

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AE31009
Course name Aerospace Structural Analysis
Offered by Aerospace Engineering
Credits 4
L-T-P 3-1-0
Previous Year Grade Distribution
7
8
7
9
7
7
5
EX A B C D P F
Semester Autumn


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE21004 3 - 1 - 0: 4 CreditsAnalysis of Aircraft Structures; Thin-walled structures based on elasticity approach; Torsion, bending and shear of open and closed thin-walled cells; Structural instability; Buckling of columns, linear and nonlinear theories, Southwell method, inelastic buckling, buckling under nonconservative forces.Books:T H G Megson, Aircraft Structures for Engineering Students, Edward ArnoldH Ashley, Engineering Analysis of Flight Vehicles, Addison WesleyC K Wang, Introductory Structural Analysis with Matrix Method, Englewood Cliffs, Prentice HallE F Bruhn, Analysis and Design of Aircraft Structures, Tri-State Offset CoE E Sechler and L G Dunn, Airplane Structural Analysis and Design, Dover


Concepts taught in class[edit | edit source]

Student Opinion[edit | edit source]

How to Crack the Paper[edit | edit source]

Classroom resources[edit | edit source]

Additional Resources[edit | edit source]



Time Table[edit | edit source]

Day 8:00-8:55 am 9:00-9:55 am 10:00-10:55 am 11:00-11:55 am 12:00-12:55 pm 2:00-2:55 pm 3:00-3:55 pm 4:00-4:55 pm 5:00-5:55 pm
Monday NC334
Tuesday
Wednesday NC334 NC334
Thursday NC334
Friday