Aircraft Structures 2 Anna University Question Papers

I am pursuing B.E. Aeronautical Engineering 8th semester in Anna University and I am preparing firstly for the Aircraft Structures-II subject for my exams as this is very typical subject for me so will you please provide me the last year question papers of Aircraft Structures-II subject of this University?

Can you provide me the syllabus of Semester V - Aircraft Structures II - B.E. Aeronautical Engineering program offered by Anna University, Chennai on which the question paper is based?

[pooja]

The syllabus of Semester V - Aircraft Structures II - B.E. Aeronautical Engineering program offered by Anna University, Chennai on which the question paper is based is as follows:

AE6502 AIRCRAFT STRUCTURES - II

OBJECTIVES:
To provide the students various methods for analysis of aircraft wings and fuselage.
To provide the behavior of major aircraft structural components.

UNIT I UNSYMMETRICAL BENDING
Bending of symmetric beams subject to skew loads - bending stresses in beams of unsymmetrical sections generalized k method, neutral axis method, principal axis method.

UNIT II SHEAR FLOW IN OPEN SECTIONS
Thin walled beams concept of shear flow the shear centre and its determination shear flow distribution in symmetrical and unsymmetrical thin-walled sections structural idealization shear flow variation in idealized sections.

UNIT III SHEAR FLOW IN CLOSED SECTIONS
Bredt - Batho theory single-cell and multi-cell tubes subject to torsion shear flow distribution in thin-walled single & multi-cell structures subject to combined bending torsion with walls effective and ineffective in bending shear centre of closed sections.

UNIT IV BUCKLING OF PLATES
Bending of thin plates rectangular sheets under compression - local buckling stress of thin walled sections crippling strength estimation thin-walled column strength load carrying capacity of sheet stiffener panels effective width

UNIT V STRESS ANALYSIS OF WING AND FUSELAGE
Loads on an aircraft the V-n diagram shear force and bending moment distribution over the aircraft wing and fuselage shear flow in thin-webbed beams with parallel and non-parallel flanges complete tension field beams semi-tension field beam theory

OUTCOMES
Ability to analyse the aircraft wings and fuselage
Ability to demonstrate the behavior of major aircraft structural components

TEXT BOOKS:
1. Megson T M G , "Aircraft Structures for Engineering Students", Elsevier Ltd, 2007
2. Peery, D.J., and Azar, J.J., "Aircraft Structures", 2nd edition, McGraw Hill, N.Y., 1999
3. Bruhn. E.H., "Analysis and Design of Flight Vehicles Structures", Tri-state off-set Company, USA, 1985

REFERENCES:
1. Rivello, R.M., "Theory and Analysis of Flight Structures", McGraw Hill, 1993.
2. Howard D Curtis, "Fundamentals of Aircraft Structural Analysis", WCB-McGraw Hill, 1997