Aircraft Structures II detailed Syllabus for Aeronautical Engineering (AERO), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.
For all other VTU AERO 6th Sem Syllabus for BE 2018 Scheme, do visit VTU AERO 6th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for aircraft structures ii is as follows.
Course Objectives:
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Module 1
Bending of Open and Closed Thin Walled Beams Symmetrical bending, unsymmetrical bending, direct stress distribution due to bending,position of the neutral axis, load intensity, shear force, and bending moment relationships, deflection due to bending, calculation of section properties, approximation for thin-walled sections.
Module 2
Shear and Torsion of Open and Closed Thin Walled Beams- General stress, strain, and displacement relationship for open and single-cell closed section thin-walled beams, shear of open section beams, shear centre, shear of closed section beams. Torsion of close section beam, and displacement associated with the Bredt-Batho shear flow. Torsion of open section beam. Combined bending, shear, torsion.
Module 3
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Module 4
Design Criteria and Structural Idealization Design Criteria, Safety Factor, Design life criteria, Analysis method, Life Assessment procedures, Design Principle, Two bay crack criteria, Widespread Fatigue damage. Structural Idealization StructuralidealizationPrinciple,Idealizationofapanel,effectofidealizationontheanalysisofopenandclosedsectionbea ms.Bendingofopenandclosedsectionidealizedbeams,shearofopensectionandclosedsectionidealizedbeams.Deflecti onofopenand closed section idealized beams.
Module 5
Stress Analysis in Wing Spars and Box beams Tapered wing spar, open and closed section beams, beams having variable stringer areas, three- boom shell, torsion and shear, tapered wings, cut-outs in wings. Stress Analysis in Fuselage Frames Bending, shear, torsion, cut-outs in fuselages, principles of stiffeners construction, fuselage frames, shear flow distribution.
Course Outcomes:
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Question paper pattern:
- The question paper will have ten full questions carrying equal marks.
- Each full question will be for 20 marks.
- There will be two full questions (with a maximum of four sub- questions) from each module.
- Each full question will have sub- question covering all the topics under a module.
- The students will have to answer five full questions, selecting one full question from each module.
Text Books:
- Aircraft Structures for Engineering Students Megson, T. H. G Edward Arnold 1995
- Aircraft Structures Peery D J & Azar J J McGraw Hill N.Y 2nd edition,1993
Reference Books:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
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For detail Syllabus of all other subjects of BE 6th Sem Aeronautical Engineering, visit (AERO) 6th Sem Syllabus Subjects.
For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.