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 โinter 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.