AS3020: Aerospace Structures
Jul-Nov, 2025

Table of Contents

Introduction

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Aircraft Structures for Engineering Students, T.H.G. Megson

Figure 1: Course Textbook: "Aircraft Structures for Engineering Students", T.H.G. Megson

Instructor, TA, and the basics

files/July_Nov_2025_final_timetable_18-07-2025.pdf

Some Planning

  • We have a total of 53 working days ahead of us. The weekly splitup is:
    • 3 Lectures: ~39 in total
    • 1 Tutorial With Faculty: ~13 in total
    • 1 Extended Tutorial With TA: ~13 in total

Evaluation Rubrics

  • One assignment will be given for each module due in one week from the date of posting.
    • Each assignment will include 2 numerical/analytical exercises and one reading exercise.
  • Two Quizzes and an End Sem occupy the examination portion.

    Evaluation Assignments Quizzes End-Sem
    Weightage 30% 30% 40%

Policies

Honor Code Policy
You are required to sign an honor code for each submission, failing which evaluation will not be done.

  • Honor Code

    Upon my honor I state that I have received no unauthorized support and can attest that the submission reflects my understanding of the subject matter.

  • Attendance Policy
    • We will enforce the institute's 75% attendance policy.
    • No one will be turned away from class, but the time of entry will be logged in the attendance application.
    • Attendance will be computed based on total minutes spent in class divided by 50 minutes.
  • Late Submission Policy
    • No late submissions will be encouraged. If you miss the deadline, you miss the submission.
    • Exceptions will be considered only if I receive written communication through Moodle before the submission date.
  • Communication Medium
    • Moodle will be used as the primary mode of communication for the class. You can also write emails, but I prefer moodle.

Module 1: Design of Aircrafts

cutler.jpg

Figure 2: Reference textbook for aircraft design overview

loads1.jpg

rivets.png

Overview

A400m.jpg

Figure 3: A400m structure

wings.png

rivet-figure1.png

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Figure 4: Fan from my home

  • Fuselage construction
    • Stressed skin design
    • monocoque, semi-monocoque, etc.
    • Pressurized vs un pressurized design
    • Stringers and stiffeners.
  • Wing construction
    • Shape requirements: lift generation from airfoil.
    • Wing ribs, spars, etc.
  • Loads on the different members.
    • Load distribution. Discuss loads for different maneuvers.
    • Load envelopes (V-n diagrams).
    • Relate global loads to local loads on members.
    • Airworthiness.
  • Joining Processes
    • Screwing, Bolting, Riveting, Welding.
    • Rivets over bolts: blind riveting, resistance to vibration, "permanence", etc.
    • Riveting process.
    • Bolt-load distribution calculations.
    • Other joining methods.
Note: The following objects have the same drag (according to laminar simulation)!

Class Slides

Old Versions

Practice Problems

  • Chapter 12 Problems in Megson.
  • Aircraft FBD from Chapter 14 in Megson.

Module 2: Aircraft Materials

sstrain.jpg

quenchedsteel.jpeg

Overview

  • Understanding the stress-strain curve.
    • Elastic regime, plastic yield, proof load, failure, elongation at failure, toughness, etc.
    • Strain hardening.
  • The need for alloys.
    • Show dramatic difference between raw Al and Al-alloy. Raw Fe & steels.
    • Outline basic considerations.
    • Examples of some common alloys with historical context.
    • Aluminum Alloys
      • Aluminum-Copper (Al-Cu) (High strength-to-weight ratio)
      • Aluminum-Magnesium (Al-Mg) (Good corrosion resistance but cracks)
      • Aluminum-Silicon (Al-Si) (Machinability)
    • Titanium Alloys
      • Titanium-Aluminum (Ti-Al) (High specific properties)
    • Nickel-based Superalloys (High temperature components)
      • Nickel-Chromium, Nickel-Aluminum
  • Fatigue
    • Failure at stress levels way below yield through repeated application.
    • Show S-n curves. Contrast behavior of Steel and Al-alloys.
  • Creep
    • Gradual increase in strain for fixed load
    • Fundamentally a high-temperature phenomenon
  • Phase Diagrams
    • Binary
      • Cu-Ni
    • Eutectic
      • Pb-Sn
    • The Iron-Carbon System
      • Equilibrium phases: $α$-Ferrite, $γ$-Austenite, $δ$-ferrite, Cementite (Fe$_3$C)
      • Non-equilibrium phases: Bainite, Martensite

Class Slides

Old Versions

Practice Problems

  • Only concepts. Chapters 11, 15 in Megson.
  • Fe-C phase diagram.

Module 3: Elasticity

B_defex.jpg

Overview

  • Fundamentals
    • Use the stress-strain curve and go into elasticity.
  • Strain
    • Introduce strain. Constitutive relationship.
    • Strain compatibility.
  • Stress
    • Derive stress-balance => governing equations.
    • Stress Mohr's circle.
  • Constitutive Relationships
    • Thermo-elasticity outline.
  • Introduction to 2D Problems. Will revisit in Module 6.

Class Slides

Old Versions

Practice Problems

  • Chapter 1 problems in Megson.
  • Chapter 1-3 problems from Sadd.

Module 4: Bending of Beams

D_full.png

Figure 5: An I-section beam subjected to 3-point bending

SXY.png

Figure 6: sigma12 section strains for an I section under bending

SXZ.png

Figure 7: sigma13 section strains for an I section under bending

Isection_17.png

Figure 8: Analytical shear flow predictions for an I section beam

Csection_V3fl.png

Figure 9: Shear flow and Shear Centre calculation for a C-sectino

Overview

  • Motivate by applications (wings, wing spars, etc.).
  • Beam theory assumptions and justifications (stringer-stiffeners, shape-preservation).
  • Unsymmetrical bending of solid beams (wings).
  • Shear of thin-walled beams (wing sections).
    • Open sections, closed sections.
    • Multi-cell closed/open combination sections.

Class Slides

Old Versions

Useful Links

Practice Problems

  • Chapter 16, 17, 20 problems in Megson.
  • Chapter 5 problems from CT Sun.

Module 5: Torsion of Beams

pristors_def.png

ellbeam_orthview_MAG.png

ellbeam_orthview_DX.png

sqsec.png

trsec.png

Overview

  • Solid section torsion.
    • Prandtl stress function.
    • Warping of section.
    • Discussion of physicality.
      • Mention St. Venant's principle, will revisit in Module 6.
  • Thin-walled torsion.
    • Closed section, open section.

Class Slides

Useful Links

  1. FreeFem++ Scripts numerically solving the Poisson problem for both stress function and warping for different solid sections.
    1. a_ellipse.edp: Ellipse section
    2. b_rectangle.edp: Rectangle section
    3. c_triangle.edp: Triangle section
    4. g_thinwalledrect.edp: (Closed) Thin-walled rectangular section
    5. h_csect.edp: (Open) C section
  2. Code_Aster Tutorial for Solid Section Torsion
    1. ellbeam.hdf : HDF file for running the FEA
  3. Wxmaxima sheet for two cell section
  4. Advanced Solid Mechanics Notes from Prof. U. Saravanan
  5. Structural Mechanics Notes, MIT AeroAstro
  6. Steel Construction Notes

Practice Problems

  • Chapter 18, 19 problems from Megson.
  • Chapter 4 problems from CT Sun.

Module 6: Variational Mechanics

Overview

  • Principle of Virtual Work
  • Primer on Calculus of Variations

Class Slides

Practice Problems

  • Chapter 4, 5 problems in Megson (only straight beam type).

Module 7: Structural Stability

wrinkl.jpg

bm_buckanim.gif

Figure 10: Animation of post-buckling of pinned-pinned/roller supported beam.

Overview

  • Column buckling.
    • Derive governing equation for column-buckling.
    • Sturm-Liouville ODE.
    • Euler buckling analysis.
  • Plate buckling.
    • Write down governing equation (derivation left for self study).
    • Show examples from aircrafts.
    • Possibility and avenue for thermal buckling from governing equations.

Class Slides

Practice Problems

  • Chapter 7, 8, 9 problems from Megson (only whatever was covered in class).
  • Class notes/assignment type problems.

References

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Last updated: 2025-10-08.