Modules / Lectures

Module Name | Download |
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noc20_ae08_assignment_Week_0 | noc20_ae08_assignment_Week_0 |

noc20_ae08_assignment_Week_1 | noc20_ae08_assignment_Week_1 |

noc20_ae08_assignment_Week_2 | noc20_ae08_assignment_Week_2 |

noc20_ae08_assignment_Week_3 | noc20_ae08_assignment_Week_3 |

noc20_ae08_assignment_Week_4 | noc20_ae08_assignment_Week_4 |

noc20_ae08_assignment_Week_5 | noc20_ae08_assignment_Week_5 |

noc20_ae08_assignment_Week_6 | noc20_ae08_assignment_Week_6 |

noc20_ae08_assignment_Week_7 | noc20_ae08_assignment_Week_7 |

noc20_ae08_assignment_Week_8 | noc20_ae08_assignment_Week_8 |

Sl.No | Chapter Name | MP4 Download |
---|---|---|

1 | Lecture 01: Introduction | Download |

2 | Lecture 02: Introduction (Cont'd) | Download |

3 | Lecture 03: Introduction (Cont'd) | Download |

4 | Lecture 04: Load Encountered by a Typical Aircraft | Download |

5 | Lecture 05: Conceptual Structural Details of a Typical Aircraft | Download |

6 | Lecture 06: Airworthiness of An Aircraft | Download |

7 | Lecture 07: Aerodynamic Loads and Load Factors | Download |

8 | Lecture 08:Loads From A Symmetric Manoeuvre Of An Aircraft " | Download |

9 | Lecture 09: Shear and Moment on Wing An Aircraft | Download |

10 | Lecture 10: Distribution Of Load On The Fuselage | Download |

11 | Lecture 11: Unit Load Analysis Of Fuselage | Download |

12 | Lecture 12: Truss System | Download |

13 | Lecture 13: Truss System (Contd.) | Download |

14 | Lecture 14: Space Structures | Download |

15 | Lecture 15: Space Structures (Contd.) | Download |

16 | Lecture 16: Wing Truss System " | Download |

17 | Lecture 17: Introduction to Energy Methods | Download |

18 | Lecture 18: Dummy and Unit Load Method | Download |

19 | Lecture 19: Dummy and Unit Load Method - Examples | Download |

20 | Lecture 20: Castigliano's Theorems | Download |

21 | Lecture 21: Rayleigh - Ritz Method | Download |

22 | Lecture 22: Statically Indeterminate Structures | Download |

23 | Lecture 23: Theory of Elasticity - Stress | Download |

24 | Lecture 24: Theory of Elasticity - Equilibrium | Download |

25 | Lecture 25: Stress Transformation and Principal Stress | Download |

26 | Lecture 26: Theory of Elasticity - Principal Stress Boundary Condition | Download |

27 | Lecture 27: Shear Stresses | Download |

28 | Lecture 28: Introduction of Strain | Download |

29 | Lecture 29: "Introduction of strain - Equations of compatibility" | Download |

30 | Lecture 30: Formulation of Elasticity Problems | Download |

31 | Lecture 31: Inverse Method of Solution | Download |

32 | Lecture 32: Semi-Inverse Method of Solution | Download |

33 | Lecture 33: Equilibrium Equation in Polar Coordinate System | Download |

34 | Lecture 34: Compatibility Condition in Polar Cordinate System | Download |

35 | Lecture 35: Effects of Circular Hole on Stress Distributions in a Plate | Download |

36 | Lecture 36: Effects of Circular Hole on Stress Distributions in a Plate | Download |

37 | Lecture 37: "Effects of Circular Hole on Stress Distributions in a Plate " | Download |

38 | Lecture 38: Theory of Elasticity - Torsion Problems | Download |

39 | Lecture 39: Theory of Elasticity - Torsion Problems (Contd.) | Download |

40 | Lecture 40: Torsion of an Elliptical Bar | Download |

41 | Lecture 41: Membrane Analogy for Torsion Problem | Download |

42 | Lecture 42: Membrane Analogy for Torsion Problem (Contd.) | Download |

Sl.No | Chapter Name | English |
---|---|---|

1 | Lecture 01: Introduction | Download Verified |

2 | Lecture 02: Introduction (Cont'd) | Download Verified |

3 | Lecture 03: Introduction (Cont'd) | Download Verified |

4 | Lecture 04: Load Encountered by a Typical Aircraft | Download Verified |

5 | Lecture 05: Conceptual Structural Details of a Typical Aircraft | Download Verified |

6 | Lecture 06: Airworthiness of An Aircraft | Download Verified |

7 | Lecture 07: Aerodynamic Loads and Load Factors | Download Verified |

8 | Lecture 08:Loads From A Symmetric Manoeuvre Of An Aircraft " | Download Verified |

9 | Lecture 09: Shear and Moment on Wing An Aircraft | Download Verified |

10 | Lecture 10: Distribution Of Load On The Fuselage | Download Verified |

11 | Lecture 11: Unit Load Analysis Of Fuselage | Download Verified |

12 | Lecture 12: Truss System | Download Verified |

13 | Lecture 13: Truss System (Contd.) | Download Verified |

14 | Lecture 14: Space Structures | Download Verified |

15 | Lecture 15: Space Structures (Contd.) | Download Verified |

16 | Lecture 16: Wing Truss System " | Download Verified |

17 | Lecture 17: Introduction to Energy Methods | Download Verified |

18 | Lecture 18: Dummy and Unit Load Method | Download Verified |

19 | Lecture 19: Dummy and Unit Load Method - Examples | Download Verified |

20 | Lecture 20: Castigliano's Theorems | Download Verified |

21 | Lecture 21: Rayleigh - Ritz Method | Download Verified |

22 | Lecture 22: Statically Indeterminate Structures | Download Verified |

23 | Lecture 23: Theory of Elasticity - Stress | Download Verified |

24 | Lecture 24: Theory of Elasticity - Equilibrium | Download Verified |

25 | Lecture 25: Stress Transformation and Principal Stress | Download Verified |

26 | Lecture 26: Theory of Elasticity - Principal Stress Boundary Condition | Download Verified |

27 | Lecture 27: Shear Stresses | Download Verified |

28 | Lecture 28: Introduction of Strain | Download Verified |

29 | Lecture 29: "Introduction of strain - Equations of compatibility" | Download Verified |

30 | Lecture 30: Formulation of Elasticity Problems | Download Verified |

31 | Lecture 31: Inverse Method of Solution | Download Verified |

32 | Lecture 32: Semi-Inverse Method of Solution | Download Verified |

33 | Lecture 33: Equilibrium Equation in Polar Coordinate System | Download Verified |

34 | Lecture 34: Compatibility Condition in Polar Cordinate System | Download Verified |

35 | Lecture 35: Effects of Circular Hole on Stress Distributions in a Plate | Download Verified |

36 | Lecture 36: Effects of Circular Hole on Stress Distributions in a Plate | Download Verified |

37 | Lecture 37: "Effects of Circular Hole on Stress Distributions in a Plate " | Download Verified |

38 | Lecture 38: Theory of Elasticity - Torsion Problems | Download Verified |

39 | Lecture 39: Theory of Elasticity - Torsion Problems (Contd.) | Download Verified |

40 | Lecture 40: Torsion of an Elliptical Bar | Download Verified |

41 | Lecture 41: Membrane Analogy for Torsion Problem | Download Verified |

42 | Lecture 42: Membrane Analogy for Torsion Problem (Contd.) | Download Verified |

Sl.No | Language | Book link |
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1 | English | Download |

2 | Bengali | Not Available |

3 | Gujarati | Not Available |

4 | Hindi | Not Available |

5 | Kannada | Not Available |

6 | Malayalam | Not Available |

7 | Marathi | Not Available |

8 | Tamil | Not Available |

9 | Telugu | Not Available |