Aircraft Structures-II detail syllabus for Aeronautical Engineering (Aero), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AE64), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.
For all other aero 6th sem syllabus for be 2017 scheme vtu you can visit Aero 6th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for aircraft structures-ii is as follows.
Course Objectives:
This course will enable students to
- Understand the concepts of open and closed thin walled beams.
- Acquire the knowledge of buckling of plates, joints and fittings.
- Comprehend the stress analysis on wings and fuselage.
Module 1
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Module 2
Combined Open and Closed Section Beams, and Structural Idealisation Bending, shear, torsion. Structural idealisation-Principle, Idealisation of a panel, effect of idealisation on the analysis of open and closed section beams. Bending of open and closed section idealised beams, shear of open section and closed section idealised beams. Deflection of open and closed section idealised beams.
Module 3
Buckling of Plates, Joints and Fittings Buckling of Isotropic flat plates in compression, ultimate compressive strength of Isotropic flat sheet, plastic buckling of flat sheet, columns subjected to local crippling failure, Needham & Gerard method for determining crippling stress, curved sheets in compression, elastic buckling of curved rectangular plates. Pure tension field beams, angle of
diagonal tension in web. Joints and Fittings- bolted or riveted joints, accuracy of fitting analysis, eccentrically loaded connections, welded joints, and concept of effective width.
Module 4
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Module 5
Stress Analysis in Fuselage Frames Bending, shear, torsion, cut-outs in fuselages, principles of stiffeners construction, fuselage frames, shear flow distribution.
Course Outcomes:
After studying this course, students will be able to:
- Utilize the concepts of thin walled beams.
- Calculate the buckling of plates.
- Analysis the stress in wings and fuselage frames.
Graduate Attributes (as per NBA):
- Engineering Knowledge.
- Problem Analysis.
- Design / development of solutions
- Interpretation of data
Question paper pattern:
- The question paper will have ten questions.
- Each full question consists of 16 marks.
- There will be 2full questions (with a maximum of four sub questions) from each module.
- Each full question will have sub questions covering all the topics under a module.
- The students will have to answer 5 full questions, selecting one full question from each module.
Text Books:
- Megson, T. H. G., Aircraft Structures for Engineering Students, Edward Arnold,1995.
- Peery D J & Azar J J, Aircraft Structures, 2nd edition, McGraw Hill N.Y.,1993
Reference Books:
- Bruhn E. F., Analysis & Design of Flight Vehicles Structures, Tri-State offset Co, USA,1985.
- Megson, T. H. G., Introduction to Aircraft Structural Analysis, Elsevier, 2nd Edition, 2014.
- Bruce K Donaldson, Analysis of Aircraft Structures, Cambridge Aerospace Series, 1992.
For detail syllabus of all other subjects of BE Aero, 2017 scheme do visit Aero 6th Sem syllabus for 2017 scheme.
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