Course10110508442 lectures
Aircraft Structures - I
Prof. Anup Ghosh · IIT Kharagpur
About
This course is an introduction for the analysis of aircraft structures. It bridges together the basic solid mechanics with applications to aerospace structures. The course starts with the introduction to the basic details of type of structures used in aircraft construction. It is followed by an introduction to the estimation of loads on wing, fuselage and landing gear. Principle of stressed skin structure and indeterminate structures are covered next. Theory of elasticity will be introduced later for analysis of problems related to aerospace structures.
INTENDED AUDIENCE : Aerospace, Mechanical, Civil, Naval Architecture.
PREREQUISITES : Basic Solid Mechanics
Lectures
Week 1
- Lecture 01 : Introduction
- Lecture 02 : Introduction (Cont'd)
- Lecture 03 : Introduction (Cont'd)
- Lecture 04 : Load Encountered by a Typical Aircraft
- Lecture 05 : Conceptual Structural Details of a Typical Aircraft
Week 2
- Lecture 06 : Airworthiness of An Aircraft
- Lecture 07 : Aerodynamic Loads and Load Factors
- Lecture 08 : Loads From A Symmetric Manoeuvre Of An Aircraft
- Lecture 09 : Shear and Moment on Wing An Aircraft
- Lecture 10 : Distribution Of Load On The Fuselage
- Lecture 11: Unit Load Analysis Of Fuselage
Week 3
- Lecture 12 : Truss System
- Lecture 13 : Truss System (Contd.)
- Lecture 14 : Space Structures
- Lecture 15 : Space Structures (Contd.)
- Lecture 16 : Wing Truss System
Week 4
- Lecture 17 : Introduction to Energy Methods
- Lecture 18 : Dummy and Unit Load Method
- Lecture 19 : Dummy and Unit Load Method - Examples
- Lecture 20 : Castigliano's Theorems
- Lecture 21 : Rayleigh - Ritz Method
- Lecture 22 : Statically Indeterminate Structures
Week 5
- Lecture 23 : Theory of Elasticity - Stress
- Lecture 24 : Theory of Elasticity - Equilibrium
- Lecture 25 : Stress Transformation and Principal Stress
- Lecture 26 : Theory of Elasticity - Principal Stress Boundary Condition
- Lecture 27 : Shear Stresses
Week 6
- Lecture 28 : Introduction of Strain
- Lecture 29 : Introduction of strain - Equations of compatibility
- Lecture 30 : Formulation of Elasticity Problems
- Lecture 31 : Inverse Method of Solution
- Lecture 32 : Semi-Inverse Method of Solution
Week 7
- Lecture 33 : Equilibrium Equation in Polar Coordinate System
- Lecture 34 : Compatibility Condition in Polar Coordinate System
- Lecture 35 : Effects of Circular Hole on Stress Distributions in a Plate
- Lecture 36 : Effects of Circular Hole on Stress Distributions in a Plate (Contd.)
- Lecture 37 : Effects of Circular Hole on Stress Distributions in a Plate (Contd.)
Week 8
Syllabus and materials
At NPTEL, as the course publishes them.
Credits and licence
- Institution
- IIT Kharagpur
- Department
- Aerospace Engineering
- Teacher
- Prof. Anup Ghosh
- Level
- Undergraduate
- Language
- English
- Subjects
- Engineering
- Source
- NPTEL
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only. NPTEL's terms
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
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