AE2254 AIRCRAFT STRUCTURES – I SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 4TH SEM SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY FOURTH SEMESTER BE AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,PREVIOUS YEAR QUESTION PAPERS,MODEL QUESTION PAPERS, CLASS NOTES, IMPORTANT 2 MARKS, 8 MARKS, 16 MARKS TOPICS. IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI,TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2254 AIRCRAFT STRUCTURES – I L T P C
3 1 0 4
OBJECTIVE
To study different types of beams and columns subjected to various types of loading and
support conditions with particular emphasis on aircraft structural components.
UNIT I STATICALLY DETERMINATE STRUCTURES 10+3
Analysis of plane Truss-Method of joints-3 D Truss-Plane frames-Composite beam.
UNIT II STATICALLY INDETERMINATE STRUCTURES 10+3
Propped Cantilever- Fixed-Fixed beams-Clapeyron's Three Moment Equation - Moment
Distribution Method.
UNIT III ENERGY METHODS 10+4
Strain Energy due to axial, bending and Torsional loads – Castigliano’s theorems-
Maxwell's Reciprocal theorem, Unit load method - application to beams, trusses, frames,
rings, etc.
UNIT IV COLUMNS 10+4
Columns with various end conditions – Euler’s Column curve – Rankine’s formula -
Column with initial curvature - Eccentric loading – South well plot – Beam column.
UNIT V FAILURE THEORY 5+1
Maximum Stress theory – Maximum Strain Theory – Maximum Shear Stress Theory –
Distortion Theory – Maximum Strain energy theory – Application to aircraft Structural
problems.
TOTAL: 60 PERIODS TEXT BOOKS
1. Donaldson, B.K., “Analysis of Aircraft Structures – An Introduction”, McGraw-Hill,
1993.
2. Bruhn.E.F.”Analysis and design of flight vehicle structures” Tri set of offset company,
USA,1973.
REFERENCE
1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co,
1990.
AE2254 AIRCRAFT STRUCTURES – I L T P C
3 1 0 4
OBJECTIVE
To study different types of beams and columns subjected to various types of loading and
support conditions with particular emphasis on aircraft structural components.
UNIT I STATICALLY DETERMINATE STRUCTURES 10+3
Analysis of plane Truss-Method of joints-3 D Truss-Plane frames-Composite beam.
UNIT II STATICALLY INDETERMINATE STRUCTURES 10+3
Propped Cantilever- Fixed-Fixed beams-Clapeyron's Three Moment Equation - Moment
Distribution Method.
UNIT III ENERGY METHODS 10+4
Strain Energy due to axial, bending and Torsional loads – Castigliano’s theorems-
Maxwell's Reciprocal theorem, Unit load method - application to beams, trusses, frames,
rings, etc.
UNIT IV COLUMNS 10+4
Columns with various end conditions – Euler’s Column curve – Rankine’s formula -
Column with initial curvature - Eccentric loading – South well plot – Beam column.
UNIT V FAILURE THEORY 5+1
Maximum Stress theory – Maximum Strain Theory – Maximum Shear Stress Theory –
Distortion Theory – Maximum Strain energy theory – Application to aircraft Structural
problems.
TOTAL: 60 PERIODS TEXT BOOKS
1. Donaldson, B.K., “Analysis of Aircraft Structures – An Introduction”, McGraw-Hill,
1993.
2. Bruhn.E.F.”Analysis and design of flight vehicle structures” Tri set of offset company,
USA,1973.
REFERENCE
1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co,
1990.
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