AE8502 Aircraft Structures โ€“ II Syllabus:

AE8502 Aircraft Structures โ€“ II Syllabus โ€“ Anna University Regulation 2017

UNIT I Unsymmetrical Bending

Bending of symmetric beams subject to skew loads โ€“ bending stresses in beams of unsymmetrical sections โ€“ generalized k-method, neutral axis method, principal axis method, Advantages and Disadvantages of three methods.

UNIT II Shear Flow In Open Sections

Thin walled beams โ€“ concept of shear flow โ€“ the shear centre and its determination โ€“ shear flow distribution in symmetrical and unsymmetrical thin-walled sections โ€“ structural idealization โ€“ shear flow variation in idealized sections-Applications of shear flow calculations.

UNIT III Shear Flow In Closed Sections

Bredt โ€“ Batho theory โ€“ single-cell and multi-cell tubes subject to torsion โ€“ shear flow distribution in thin-walled single & multi-cell structures subject to combined bending and torsion โ€“ with walls effective and ineffective in bending-Importance of shear flow & shear center determination.

UNIT IV Buckling Of Plates

Bending of thin plates โ€“ local buckling stress of thin walled sections โ€“ crippling strength estimation thin skin stringer panel-effective skin width โ€“inter rivet buckling-skin stringer panel-Integrally stiffened panels-cutouts- Lightly loaded beams.

UNIT V Stress Analysis Of Wing And Fuselage

Aircraft loads- classification โ€“ the V-n diagram โ€“ shear force and bending moment distribution over the aircraft wing and fuselage โ€“ shear flow in thin-webbed beams with parallel and nonparallel flanges โ€“ complete tension field beams โ€“ semi-tension field beam theory.

AE8502 Aircraft Structures - II Syllabus