Aircraft Structures – II Syllabus for B.Tech 5th sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.<\/p>\n
The detailed syllabus for Aircraft Structures – II B.Tech (R13) fifthsem is as follows<\/p>\n
OBJECTIVES<\/strong>:<\/p>\n UNIT I : UNSYMMETRICAL BENDING \u00a0<\/strong>\u00a0 \u00a0[9 hours] UNIT II : SHEAR FLOW IN OPEN SECTIONS<\/strong> \u00a0 \u00a0\u00a0[9 hours] UNIT III: SHEAR FLOW IN CLOSED SECTIONS<\/strong> \u00a0 \u00a0[9 hours]\n
\nBending of symmetric beams subject to skew loads – bending stresses in beams of unsymmetrical\u00a0sections \u2013 generalized \u2018k\u2019 method, neutral axis method, principal axis method.<\/p>\n
\nThin walled beams \u2013 concept of shear flow \u2013 the shear centre and its determination \u2013 shear flow\u00a0distribution in symmetrical and unsymmetrical thin-walled sections \u2013 structural idealization \u2013 shear\u00a0flow variation in idealized sections.<\/p>\n
\nBredt – Batho theory \u2013 single-cell and multi-cell tubes subject to torsion \u2013 shear flow distribution in\u00a0thin-walled single & multi-cell structures subject to combined bending torsion \u2013 with walls effective and\u00a0ineffective in bending \u2013 shear centre of closed sections.<\/p>\n