AE404PC: Analysis of Aircraft Structures AE Syllabus for B.Tech 2nd Year 2nd Sem R18 Regulation JNTUH

Analysis of Aircraft Structures detailed syllabus for Aeronautical Engineering (AE), 2nd Year 2nd Sem R18 regulation has been taken from the JNTUH official website and presented for the B.Tech students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. We make sure the result links and syllabus uploaded here is latest and up to date, also the syllabus PDF files can also be downloaded from the universities official website.

For Aeronautical Engineering (AE) 2nd Year 2nd Sem R18 Regulation Scheme, do visit AE 2nd Year 2nd Sem R18 Scheme. The detailed syllabus for analysis of aircraft structures is as follows.

Analysis of Aircraft Structures Subject Syllabus for AE 2nd Year 2nd Sem R18 Regulation

Pre-Requisites:

For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdf platform to make students’s lives easier.
.

Course Objectives:

Understand the aircraft structural components and its behavior under different loading conditions.
Obtain knowledge in plate buckling and structural instability of stiffened panels for airframe structural analysis.
Explain the thin walled section and structural idealization of panels and differentiate from the type of loads carried.
Solve for stresses and deflection in aircraft structures like fuselage, wing and landing gear.

Course Outcomes:

Types of structure used in aircraft and various loads experienced by components

UNIT – I

UNIT – II

Thin Plate Theory, Structural Instability: Analysis of thin rectangular plates subject to bending, twisting, distributed transverse load, combined bending and in-plane loading: Thin plates having small initial curvature, energy methods of analysis. Buckling of thin plates: Elastic, inelastic, experimental determination of critical load for a flat plate, local instability, instability of stiffened panels, failure stresses in plates and stiffened panels. Tension field beams- complete diagonal tension, incomplete diagonal tension, post buckling behaviour.

UNIT – III

Bending, Shear and Torsion of Thin Walled Beams: Unsymmetrical bending: Resolution of bending moments, direct stress distribution, position of neutral axis; Deflections due to bending: Approximations for thin walled sections, temperature effects; Shear loaded thin walled beams: General stress, strain and displacement relationships, direct stress and shear flow system, shear centre, twist and warping. Torsion of beams of closed section: Displacements associated with Bredt-Batho shear flow; Torsion of open section beams; Warping of cross section, conditions for zero warping; Bending, shear, torsion of combined open and closed section beams.

UNIT – IV

UNIT – V

Analysis of Fuselage, Wing and Landing Gear: Wing spar and box beams, tapered wing spar, open and closed sections beams, beams having variable stringer areas; wings – three boom shell in bending, torsion and shear, tapered wings, deflections, cutouts in wings; Cutouts in fuselages;
Fuselage frame and wing rib; principle of stiffener, web constructions. Landing gear and types; Analysis of landing gear.

TEXT BOOKS:

T. H. G. Megson, Aircraft Structures for Engineering Studentsll, Butterworth-Heinemann Ltd, 5th Edition, 2012.
E. H. Bruhn, Analysis and Design of Flight vehicles Structuresl, Tri-state off set company, USA, 4th Edition, 1965.

REFERENCE BOOKS:

For detailed syllabus of all the other subjects of B.Tech 2nd Year Aeronautical Engineering (AE), visit Aeronautical Engineering (AE) 2nd Year Syllabus Subjects.

For results of Aeronautical Engineering (AE) 2nd Year 2nd Sem R18 Regulation, visit AE 2nd Year 2nd Sem R18 Regulation results direct link.

InI JNTUH