Aircraft Structures II detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8502), Category (PC), Contact Periods/week (5), Teaching hours/week (3), Practical Hours/week (2). The total course credits are given in combined syllabus.
For all other aero 5th sem syllabus for be 2017 regulation anna univ you can visit Aero 5th Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for aircraft structures ii is as follows.”
Course Objective:
- To provide the behavior of loads experience of aircraft indigenous components.
- To provide the students adopt with various methods for analysis of aircraft wings and fuselage.
- To provide conception design of major aircraft structural components.
- To provide the better understate the low weight structures.
Unit I
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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-Applications of shear flow calculations.
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 and multi-cell structures subject to combined bending and torsion – with walls effective and ineffective in bending-Importance of shear flow and shear center determination.
Unit IV
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Unit V
Stress Analysis of Wing and Fuselage
Aircraft loads- classification – 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.
Course Outcome:
- Ability to understand loads acting an aircraft.
- Ability to identify& resolve the structural design& its limitations .
- Ability to improvise distribution their loads on aircraft member with safer limits.
- Ability to understand the design of low weight to high strength panel member.
- Ability to analyze the aircraft real structural components such as wings and fuselage.
Text Books:
- Bruhn. E.H., “Analysis and Design of Flight Vehicles Structures”, Tri-state off-set Company, USA, 1985.
- Megson T M G , “Aircraft Structures for Engineering Students”, Elsevier Ltd, 2012
- Michael Chun-Yung Niu, Airframe structural Design ,Conmilit Press Ltd,1998
References:
- Howard D Curtis, “Fundamentals of Aircraft Structural Analysis”, WCB-McGraw Hill, 1997
- Rivello, R.M., “Theory and Analysis of Flight Structures”, McGraw Hill, 1993.
- Peery, D.J., and Azar, J.J., “Aircraft Structures”, 2nd edition, McGraw – Hill, N.Y., 1999
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 5th Sem syllabus for 2017 Regulation.
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